Circuit Theory ISBN 9788184315271 ·All rights reserved wHh Techn;col Publ;cciijons. No pon of !his book should be reproduced in any form, Electronic. Mechoniccl, Phoux:opy or any informolioo sloroge ond retrievol system without prior permission in writing, from Techn.icol Pvblicotions, Pune.
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Table of Contents ..
Chapter -1 Basic Circuit Analysis an'd
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· Network Reduction TechniqUII!!'
(1~1lto(1-102l
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1.1 Introduction ......................................................................................... 1 - 1
1.2 Network Terminology ............................................................................1 - 1 1.2.1 Network ....... .
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. .. . 1-1
1 2 2 Network Element
1- 1
123Brancb
1-2
~winiL-~~~~~~~----~~~~~~~~~~-i 1~ -2
125Node
1-2
1.2.6 Mesh (or Loop) . ........... ... ...... . ... .... . . . ......................... 1 -2 1 3 Classification of Elec!dcal Networks
1-2
1.4 Energy Sources ...................................................................................1 - 4 1.4.1 Voltage Source . ................................. ... .................... 1-4 1 4 2 Curmnt Soume
1-5
1.4.3 Dependent Soutees.... . . ... ...... . ............. . . .. ... ...... .. .... . ... .. 1-6
1.4.4 RegutaUon and Loading of Soutees ........................... .. . ........... 1-7 1 50hm's I aw 1 5 1 I imitations of Ohm's 1aw
1-8 ; 1-9
1.6 Unear ive Parameters (R, Land C) ............................................ :.1 - 9 1.6.1 Resistance and its V-1 RelationshiP ............. ....... ..................... 1 - 9 1.6.21nductance and Its V.J Relallonshlp ..... . . ... .. . . .. ...... . ....... .... . ... ... 1 - 10 1.6.3 Capac!tance and Its V-1Relationship ... ... ................ . ................ 1 - 10
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1.7 Analysis of Series Circuits ................................................ .................. 1 - 12 1 7 1 Resjs!ofS in Serills 1 7 1 1 Characteristics of Series Cjtcuj!s
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1 7 2 Inductors jn Series
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1.7.3 Capacitors in Series ... . ...... ....................... ... .. .. . •·..•. : ...... 1"15
1.8 Analysis of Parallel Circuits............................................... .................. 1 - 16. 1 8 1 Reslslors in ParaDe! 1 8 11 Cbaractmistics of ?araftel Clmrjrs
1 8 2!oductors jo Parallel
1-16 1-17 1-18
1.8.3 Capacitors in ParaDe!.................................................... 1- 19
1.9 Short and Open Circuits.................................................... .................. 1 - 22 1 9 1 Short CjrQ!il
1-22
1.9.2 Open Circuit . .... . ..... ..... .... ..... . .... ....... .. . .... . .. . ... . ... . . . 1• 22 1 9 3 Redundant Branches and CQmbjnatjons
1 -23
1.10 Voltage Division In Series Circuit of Resistors .................................1 - 24 1 11 Current D ivision in Parallel Circuit of Rllsistors
1-25
1 12 Sn••rce Tra n sformation
1 -27
1 13 Combinations of Sources
1 - 30
1.13.1 VoitageSources inSeries .......... . ...... . . . .. . . . . .. . . .. . .. .. .. . . ... . .. 1-30 1.13.2 Voltage Sources in Parallel ...... . .......... . .. . ............. . .. . . . .. .... 1• 31 1 13 3 Current Sources in Series
1-31
1134 Current Sources jn Paralfel
1 - 31
1.14 Kirchhoffs Laws
1 -32
1.14.1 KIIchhotrs Current Law (KCL) .... . ... . ...... .... . . ...... . . .. .... . . ... .. .. 1-32 1.14.2 Kirthboffs Voltage Law (KVL) .• . ...•. . . . . •.. : .•...... . ..... • ............. 1· 33 1.14.3 Sign Conventions to be Followed while Applying KVL . . .. ... ..... . . .. . . . . . . .. . 1• 33 1.14.4 Aopfication of KVL to a Closed Path . . . ....... .. ... . . ... . ......... .. ....... 1• 34 1.14.5 Steps to Apply Kircllhoffs Laws to Get Network Equations ... . ...... . .......... 1. 35
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1.16 Cramer's Rule .................................................................................. 1 - 37 1 16 A C Fundamentals
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1 16 1 Instantaneous Value
1 • 40
1 162Wayetonn
1-40
1.16.3Cyde . . . . .. . . . ... . .... . . . . . ...... . . ... . . .... . .. ..... . .. . . .... . . . . . .. 1·40 1.16.4 Time Period (!) . . . . . .. . . . . . . . . . . . ... .. . . . . .... . .. . .. . . . .. . . . .. . . ..... . 1 • 40 1.16.5 Frequency (0 ... . . .. ...... .. ........ . .... . . .... .. .... ...... .. . . . . . . ... 1 • 40 1.16.6Ampli!ude. . ... .... . . .. .. . .. . . . . ... . ...... .. . .. .. . ....... . ........ . . .. 1-41 1.16.7 AngularFrequency (ru) ...... . . . ..... . .. . . . .. .... . . . ....... . ............ 1-41 1.16.8 Equation ofan Alternating Quantity... ... .. .. . . .. ... . ......... . ... .... .. .. . 1 • 41
1.17 Phasor Representation of an Alternating Quantity............................ 1-42 1.18 Concept of Phase of an Alternating Quantity .................................... 1 - 44 1 18 1 Phase Qifference
1 -46
1.18.2Phasor0iagram... . .. .. . . .. . . .... ... .. . .......... . . ...... .. ....... . ... 1-48
1.19 Mathematical Representation of Phasor ..........................................1 - 50 1.20 Multiplication and Division of Phasors ...............................................1 - 53 1.211mpedance ....................................................................................... 1 - 53 1 22 Power EactoL...-------------------.1...=.~ 1 23 Power
1-56
1.24 Series R-L-C Cjrcujt.. .., ..... ,, ... ..,, ,. ...
1-56
1 25 A C Parallel Circuit
1-58
1.25.1 Current Division for Parallel Impedances .•.••......••• • .•. . . .• ••• .• .• ... •• . 1 · 59 1.25.2 Concept of ittance . . . . . .. . . . ........ . . . . ..... .. ..... .. .. . ... ... . . . . 1-59 1.25.3 Components of ittance .... .. .... . .......... . .. .. . ... . . . .. . . . . .. ... . . 1 • 59 1.25.4 Conductance (G) . .. . . . . . .. . .. . .. .. . .... . ......... . ... . . . . .. . ... .. . . . . ."1 • 59 1.25.5 Susceptance (B) . . ...... . . .. . . . ....... . ... ....... . .'.. . .. . .. . .. ........ 1 • 60 1 26 Star and Delta Connection of Resistances 1 26 1 Pella-Star TransfO!!Da!joo
1-63
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1.26.2 Star-Delta Transfonnation . . . ...... .... . .. . .. . .. ...... . ....... . .. . ..... . . 1 • ~
Examples with Solutions ......................................................... ..................1 - 72 Review Questions .. ......... .............. ·:. . .., .............. ... , .., ....... .1 - 97
2 1 !ntroductjoo
2- 1
2.2 Loop Analysis or Mesh Analysis ..........................................................2 - 1 2.2.1 Points to for loop Analysis ...................................... 2 - 2 2.2.2 Supermesh .. .... .. .. .. ... . .. ..... .. ...... ..... ... ...... .. . . ......... .. 2 • 2 2.2.3 Steps lor the loop Analysis .. . . .... . . ... . . . . ... . . ... . ... . .. . ... . .... .. . ... 2 - 3
2.3 Node Analysis ................................................................... ....................2 - 6 2.3.1 Points to for Nodal Analysis . . .. . .. . .... ... .. . ... .. .......... . .... 2-7 2.3.2 Supemode . . . .. ... . .. . . .. ... . .... .. . .... .. .... .. ... . . ... .... . ...... . .. 2- 7 2.3.3 Steps lor the Node Analysis............... ... ........ . . . .... . .......... . . . 2 - 8
Examples with Solutions ...........................................................................2 - 11 Reyjew Ouestjoos
3 1 lntroductjoo .
2 - 39
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3-1
3.2 Superposition Theorem ..................................................... ...................3 - 1 3.2.1 Explanatlon of Superposition Theorem ...... ..... .... .. .. .. .. . .............. 3 - 1 3.2.2 Steps to Apply Superposilion Theorem .. .... .... .. . .. ...... ... ... ....... .... 3 - 3
3 3 Theyeojn's Theorem
3-8
3.3.1 Explana!ion of Thevenln's Theorem . ... . . . ... . .... . ..•.... . .. • •..... ...... .• 3- 8 3.3.2 Steps to Apply Thevenin's Theorem............................. . ........... 3- 9 3.3.3 Method of Ca!Cillating Z,. for Network with Dependent Sources . ... • • . .. . •.• ... . • 3- 11 3.3.4 Limitations of Thevenln's Theorem. . . . . . . . . . . . . . . . . . . . . . . . . . .
3 4 Norton's Theorem
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3.4.1 Explana!ion of Norton's Theorem ............... .. .. . ... . ..... . ............ 3-16
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3.4.2 Steps to Apply Norton's Theorem ..... . . ............. . .... . .. ..... ...... ... 3-18
3- 5 Maximum Power Transfer Theorem
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3.5.1 Explanalion of the Maximum Power Transfer Theorem . . •. . • o... . .. . o.. ... . ... 3 o21 3 5 2 Proof of Maximum Power Transfer Theorem
3-22
3.5.3 Corollaty . . .. . . . . ......... . ....... .. ......... . .. .. ...... o. ... ... . ..... 3 ° 24 3.6 Reciprocity Theorem ................
0 . . 0 . . . . . . . . . . . . . .. . .. . . . . . . . . .. .. . . . . . . . . . . . . . . . . . . . .. .. . .
3 - 27
3.6.1 Explanation of Reciprocity Theorem .. . .. . ..... . . ... .... . .. . ..... • • ....• . • •• 3 • 21
3.6.2 Proof of Reciprocity Theorem ...•... . ...... .. •.• ... .• •......... • • .. ••• . •. • 3 • 21 Examples with Solutions ...........................................................................3 - 32 Revjew Ouestjoos
3 - 81
4 1 Introduction
4- 1
4.2 Q-Factor or Figure of Merit ...................................................................4 - 1 4-3
4 3 Series Resonance
4.3:1 Phasor Diagrams.. . . . .... .... ..... .. .......... .... .. .. ....... . ...... . ... 4 ° 4 4
3 2 Reactance C'UVfS
4 o5
4.3.3 Variation of Impedance, ittance and Current with Frequency ......•........•.. 4 • 6 4.3A 0-Factor of Sedes Resonant Circutt, . , . .. . , , , .. . .. , , , , . , .. . , . , .... , . , . .. , . , . 4 o7 4.3.5 Voltages across Land C at Rasonance ... . . . ... ...... .... ... ...... .. . . .. . . .. 4 . 8 4.3.6 Frequendes for Maximum Voltage across Land C... . .... . ...... . ..
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4.3.7 lmpedanoa of Sedes Rol.C Circuit ln of a ... .... .... ... .. .... o. . . . • . • . •. 4 -1 3 4.3.8 Bandwidth and Selectivity . . ... ...... . . . . ...... . . . ... .. ............ . ...... 4 o14 4.3.9 Effect of GeneJator Resistanoa on Bandwidth and Selectivity . • .. •..• . o.. .. •.• . •. 4 °18
4.4 Parallel Resonance .......................................
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4 21 o
4.4.1 Variation of SUsceptance l'.ilh Frequency . . . . . ..... .. .... . .. . . . ... . ... . ...... 4 ° 25
4.4.2 The Impedance of ParaUel Resonant Circuit near Resonance .........•.......... 4 ° 27 4.4.3 Selecllvity and Bandwidth . ... . . ..... ... .. . . . . .... . . .... ... .. . ... . ..... ... 4 o30
4.4.4 Effect of Generator Resistaooe on Bandwidth and Selectivity . .... . . . . . ••• •. ... •. 4- 31
4.4.5 Currents through Land C under Antiresonanoe . . . . . ... . . . . .. . .. . .. . . . ........ 4-33 Examples with Solutions ........................................................................ .. 4 - 34 Review Questions
. 4 ·-49
51 lntmducti......._ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _........,:...J
5.2 Magnetically Coupled Circuit ................................................................5- 1 5.2 1 Self Inductance 5.2.2 Mutual inductance . .. . .. ..... ... . .. . ............ . ... . . . . ........ . .... . ... 5 - 3
5.2.3 Coefficient of Coupling or Magnetic Coupfing Coefficient (k) . . .. ...• .. ....... . . ... 5-6 5 3 Dot Conyentjons
5-8
5.4 Inductive Coupling in Series ............................................ ..................5- 13
5.4.1 Series Aidlng ............... .. ..... . .................... . ... . ......... 5 - 13 5.4.2 Series Opposing . . . . . . . .. .. . . . . . . .. . .. . .... . ....... ... .. . . ... . ... ..... 5 -14
5.5 Inductive Coupling in Parallel .............................................................. 5- 14
5.5.1 Parattel Aiding . . . . . . . . • . . . . .. . . . ... . . . .. . . . . ......... ... . ..... ...... . 5 • 15
5.5.2 Parallel Opposing .... . ...... .. .... . . .. ... .. . ..... .. . . ..... . ...... .. .... 5 • 16 5.6 Energy in a Pair of Coupled Coils .......................................................5- 18 5.7 Cond~,;ctively Coupled Equivalent Circui\.. ..........................................5- 18 5 8 I jnear Transfooner
5-20
5.9 Ideal Transformer
. .. .. 5-21
5 10 T ~.med Cjrcujts .
5-24
5.10.1 Single Tuood Circuit . .. ....... . .................... . ..... ... ... ....... . 5- 24
5 10 2
Double nrned Clrcujt
5·27
Examples with Solutions ...........................................................................5 - 33 Hev.iew Questions
5-56
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........ 6-1
6 1 Introduction ...... .. . ... .... .........
6.2 Review of Differential Equations ...........................................................6 - 1 6 3 General and Particular Solutions
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6.3.1 Homogeneous Equation . ... ... . . . .. ... .. .. . . . .. . . .. . . . ... . . . . .. .. .. . . . . . . 6- 2 6.32 Non-homogeneous Equation ...... . .. .. .. . . . . ... . . .. ... . . ... .. . . . . ... ... .. 6 • 3 6 4 Initial Conditions in Network
6-4
6 5 Initial Conditions in Network Elements
6 -5
s s1 Resistor
6-5
6 5 2 Inductor
6 -5
6.5.3 Capacitor .... ... ......... ... ....... ..... ........... . .................. 6 • 6 6.6 Step Response of Series R-L and Series R-C Circuits .........................6- 8
6.6.1 Step Response of Driven Series R·L Circuit. . ..•.. . . .• .. . . ... . •. . . . .... . . . .. . . 6 • 9 6.62 Step Response of Driven Series R.C Circuit. . .. . .. . . . . ...... . .......... ... .. . 6 • 14
6.7.1 Curren! Decay in Source Free Series R·L Circuil. ....... .. .... . . . . .... ... . . . . . 6- 20 6. 7.2 Discharne of capacitor through Resistor in Source Free Series R.C Circu~ . . ...... . 6 • 23
6.8 Step Response of Series R-L-C Circuit ......................... ....................6 - 28 Examples with Solutions .............................................. ......... ....................6 - 34 Review Questions ................................................................. .................... 6 - 43
7 1 Introduction
7. 1
7.2 Definition of Laplace Transform ............................................................7 • 2 7.3 Properties of Laplace Transform .................................... ......................7- 3 7.3.1 Unearity .. . . ....... .. . ............... .... .. . .......... . .. .. ........... 7 • 3 7.3.2 Scafing Theorem (Multiplication by t) ......... . ... . . . . .. . . ... . .. .. .......... . 7 • 4
7.3.3 Real Differenliation (Differentiation in Time Domain) .... . . .. .. ..•... . . . ........ . 7. 4
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7.3.4 Reallntegralion . •.. . ...... . ... . ..... . . .. • .. . . . . • . ..•.....•..••.....• . •. 7 • 4 7.3.5 Differentiation by s (Multiplication by t) . . . . . . . . ....... .. . . ..... . •.. . . . .. .. .• . • 7 • 5 7.3.6 Complex Translation...... .. ... . .. .. . . . . . .. . .... . .... .. . . . . ..... . .. . .... . 7 • 5 7.3.7 Real Translation (Shifting Theorem) . ... . ..• •. •..••.•••.•.. . ..•••.. .• ••••..•. 7 • 5 7.3.8 lniUal Value Theorem . . . . . .... . ... . . .. .. ........... , . . . . . . . . .. . . . . . . . 7. 5 7.3.9 Final Value Theorem ....... .. . .... . . ·.. . .... . .................. . .. . . ... .. 7 . 6
7 4 Standard.JJme.Euncti.ons.. _______.. _ ... _••••••_. ___-·········-··-~····-··..1....:....10 7.4.1 Step Function .... . ...... . .......... ....... ... .... . .. ... . .. .. ......... . 7-10 7.4.2 Ramp Function . . . ... ...... . . . . . . . .. . . .. ... .... . . . . . .... . . . ... .. . ... . . . 7-1 3 7.4.31mpulse Function ...• . . . . . ..... . ..... . . . ... • . • . . . . .. •• . ....... • .. .• ..•. . 7 - 17 7.4.3.11mportant Properties of Impulse Function . • • • . . • . . . . • . . • . . . 7-19
7.5 Relationships between Standard Time Functions...............................?- 20 7.5.1 Relation between Unit Step and Unit Ramp ..... ..... . ........ . .............. 7 • 20 7.5.2 Relation batween Unlt Step and UnH Impulse ... . ..... .... ...... ...... ... .. ... 7 • 20
7.6 Laplace Transforms of Standard Functions ........................ ................7- 21 7.6.1 Step Function ..... . .... . . . .. .... . ....... ......... . . ...... . ......... . .. 7-21 7.6.2 Ramp Function ............. . ... . ....................... .. . .. . .. . . ..... 7 • 22 7.6.31mpulse Function ............ . ... . ................. . ...... . . . .......... . 7 • 23
7.7 Laplace Transform of a Periodic Function ..........................................7- 25 7.81nverse Laplace Transform .................................................................? - 26
7.8.1 Simple and Real Roots ......... . ................ . . .... . .•..•.••.•...• • • . 7 • 27 7.8.2 Multiple Roots . .. ... ..... ... .. ........ . ............ . .................. 7 • 29
7.8.3 Complex Conjugate Roots . ... . . . . .. . . .. .. ..... . . . .. . .. . . . ....... .. ... . . . . 7 • 31
7.9 Special Case of Inverse Laplace Transform .......................................7 - 33
7.10 Inverse Laplace Transform using Convolution lntegral.. ...................7- 34 7.11 Solving Differential Equations ..........................................................7 - 38 7.12 Including Initial Conditions in the Equations .................... ................?- 40 7.13 Network Analysis using Laplace Transform .....................................?- 42
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7.13.1 Single Resistor in Laplace Domain. .. .. . ..... . • . . . . . . • . . .. .•. . • .. ... .. . • . • 7 • 42 7.1 3.2 Single Inductor in Laplace Domain............................. .. ......... 7 • 43 7.1 3.3 Single Capacnor in Laplace Domain . ..... .. .................... ... .... . .. 7 • 44 7 13 4 s Domain Netwodc
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Examples with Solutions ...........................................................................7 • 46 Review Questions
7-63
8 1 Introduction
8- 1
8.2 Advantages of Three Phase System ................................................... 8 - 2
8.3 Generation of Three Phase Voltage System ....................................... 8 - 2 8.4 Important Definitions Related to Three Phase System ........................ 8- 4
8.5 Three Phase Supply Connections ....................................................... 8 - 4 •.
8.5 1 Star Connedion . . . . .
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8.6 Concept of Line Voltages and Line Currents ....................................... 8 - 5
8.7 Concept of Phase Voltages and Phase Currents ................................ 8 • 6 8.7.1 Balanced Load . . . . . . . . . . .. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 8. 8
8.8 Relations for Star Connected Load
8-8
8 9 Relations for Delta Connected I oad
8 - 12
8.10 Power Triangle for Three Phase Load ............................................. 8 - 15 8.11 Steps to Solve Problems on Three Phase Systems ......................... 8- 15 8.12 Solution of Unbalanced Load ........................................................... 8 - 23 6 12 1 Unbalanced Three Wire Star Connected I oad
8-25
8.12.2 Unbalanced Four Wlnl Star Connected Load.... .. . . . .. . .... .. ... .. . .. ..... . 8 • 26 8.12.3 Unbalanced Delta Connected Load .. .. .. .. .. .. .. .. .. .. .. . .. .. . . • .. .. .. .. . 8 - 26
8 13 Three Phase Power Measurement
8-29
8 14 About Wattmeter
8-29
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8.15 Examples of Wattmeter Connections and Corresponding Readings .................................................................. 8 - 30 8 16 Two Wattmeter Method
8 - 32
8 16 1 Proof of Tv«> Wattmeter Method
8. 32
8.17 Power Factor Calculation by Two Wattmeter Method ...................... 8-38 8.18 Effect of P.F. on Wattmeter Readings ................................•............ 8-39 8.19 Reactive Volt-Amperes by Two Wattmeter Method ......................... 8-41 8.20 Advantages of Two Wattmeter Method ............................................ 8-42 8.21 Disadvantages of Two Wattmeter Method ....................................... 8 - 43 Examples with Solutions ...........................................................................8 - 44 Review Questions
8 - 62
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Basic Circuit Analysis and Network Reduction Techniques 1.1 Introduction The Olun's law can be successfully applied to the various circuit.• to analyse them. But in practice, the circuits may consist of one or more sources of e.m.f. and number of electrical parameters, connected in different ways. The different electrical parameters or elements are resistors, capacitors and inductors. The combination of such elements alongwith various sources of energy give rise to complicated electrical circuits, generally referred as networks. The circuit and network are used synonymously in the electrical literature. The network analysis or circuit analysis means to find a current through or voltage across any branch of network or circuit.
In circuit analysis, many a times it is necessary to reduce the complicated electrical network to simple form. In this chapter, some network simplification techniques such as source transformation, application of l
1.2 Network Terminology In this section, we shall define some of the basic which are commonly associated with a network.
1.2.1 Network Any art"'..ngement of the various electrical energy sources along with the different circuit elements is called an electric~l network. Such a network is shown in the Fig. I.L
1.2.2 Network Element Any Individual circuit element with two terminals which can be connected to other circuit clement, is called a network element. Network elements can be either active elements or ive clements. Active clements arc the clements which supply power or energy to the network. Voltage source and cu.rrcnt source are the examples of active clements. ive clements are the clements (1 - 1)
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1-2
Circuit Theory
Basic Circuit Analysis & Network Reduction Techniques
which either store en~.gy or dissipate energy in the form of heat. Resistor, inductor and capacitor are the three basic ive element:;. Inductors and capacitors can .;tore energy and resistors dissipate ener!lY in the form of heat.
1.2.3 Branch A part of the network which connL'Cts the various points of the network with one another is called a branch. In the Fig. 1.1, AB, BC, CO, OA, DE, CF and EF are the various branches. A branch may consist more than one clement.
1.2.4 Junction ?oint A point where three or more branches meet is called a junction point. Point 0 and C are the junction points in the network shown in the Fig. 1.1.
1.2.5 Node A point at which two or more elements a.re ed together is called node. The junction poinl~ are also the nodes of the network. In the nel:\vork shown in the Fig. 1.1, A, 8, C, D, E and F are the nodes of the network.
1.2.6 Mesh (or Loop) R, A
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R,
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Fig. 1.1 An electrical network
Mesh (or Loop) is a set of branches forming a closed path in a network in such a way that if one branch is removed then remaining branches do not form a closed path. A loop also can be defiru.od as a dosed path which originates from a particular node, terminating at the same node, travelling through various other nodes, without travelling through any node twice. In the Fig. 1.1 paths A-B-C-D-A. A·S.C·F·E·D·A, D·C·F·E·D etc. are the loops of the network. In this chapter, the analysis of d.c. circuits consisting of pure resistors and d.c. sources is included.
1.3 Classification of Electrical Networks The behaviour of the entire network depends on the behaviour and characteristics of Its elements. Based on such characteristics electrical network can be classified as below : I) Linear network : A circuit or network whose parameters i.e. elemenlts like resistances, inductances and capacitances are always constant irrespective of the change in time, voltage, temperature etc. is known as linear network. The Ohm's law can be applied to such network. The mathematical equations of such network can be obt.rined by using the
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Circuit Theory
1•3
Basic Circuit Analysis & Network Reduction Techniques
law of superposition. The response of the various network elements is linear with respect to the excitation applied to them. II) Non linear network : A circuit whose parameters change their values with change in time, temperature, voltage etc. is known as non linear network . The Ohm's Jaw may not be applied to such network. Such network does not follow the law of superposition. The response of the various elements is not linear with respect to their excitation. The best example is a circuit consisting of a diode where diode current does not vary linearly with the voltage applied to il Ill) Bllater.lll network : A circuit whose characteristics, behaviour is same irrespective of
the direction of current through va.rious elements of it, is called bilateral network. Network consisting only resistances is good example of bilateral network. lv) Unllater.lll network : A circuit whose operation, behaviour is dependent on the direction of the current through various elements is called unilateral network. Circuit
consisting diodes, which allows flow of current only in one direction is good example of unilateral circuit. v) Active network : A circuit which contains at least one source of energy is called active. An energy source may be a voltage or current source. vi) ive network : A circuit which contains no energy source is called ive circuit This is shown in the Fig. I .2.
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(a) Active network
(b) ive n8twork
Fig. 1.2 vii) Lumped network : A network in which all the network elements are physically separable is koown as Jumped network. Most of the electric networks :ue lumped in nature, which consists elements like R. L, C, voltage source etc. viii) Distributed network : A network in which th.e circuit elements lil<e resistance, inductance etc. cannot be physically reparable for analysis purposes, Is called distributed network. The best example of such a network is a transmission line where resistance, inductance and capacitance of a transmission line are distributed all alo-ng its length and cannot be shown as a separate elements, any where in the circuit.
Copynghtcd materia
Cln:ult Theory
1 -4
Basic Cln:ult Analysis & Network Reduction Techniques
The classification of networks can be shown as, Electrical circuits or networks
I
I
ive
Linear
Nonlinear
Unilaleral
Bilaleral
Lumped
Distribuled
Fig. 1.3 Classification of networks
1.4 Energy Sources There are basically two types of energy sources ; voltage source and current source. These are classified as i) Ideal source and ii) Practical source. Let us see the difference between ideal and practical sources.
1.4.1 Voltage Source Ideal voltage source is defined as lhe energy source which gives constant voltage across its terminals irrespective of lhe current drawn through its terminals. The symbol for ideal voltage source is shown in the Fig. 1.4 (a). This is connected to lhe load as shown in Fig. 1.4 (b). At any time lhe value of voltage at load terminals remains same. This is indicated by V- I characteristics shown in lhc Fig. 1.4 (c). ll
v,
+
0~-------------- 'L (a) Symbol
(b) Circuit
(c) ChuocterlaUca
Fig. 1.4 Ideal voltage source Practical voltage source :
But practically, every voltage source has small internal resistance shown in series wilh voltage source and is represented by R.., as shown in the Fig. 1.5. lnlemal
resistance R,.
IL
VL +
Wl>eilc!Mfe is no
'?.a
v
y;y~
Praclical Q L__ _ _ _ __
(a) Circuit
IL
(b) Characteristics
Fig. 1.5 Practical voltage source Copy(ghlcd malcri~
1·5
Circuit Theory
Basic Circuit Analysis & Networil
~eduction Techniques
Because of the R,., voltage across tenninals decreases slightly with increase in current and it is given by expression,
.-----------------------,
Key Point : For ideal voltage source, R,., = 0
Voltage sources are further classified as follows, I) Time Invariant sources :
•
£ v.=...
The sources in which voltage is not varying with time are known as time invariant voltage sources or D.C. sources. These arc denoted by capital letters. Such a source is represented in the Fig. 1.6 (a).
-r.____....,.
Fig. 1.6 (a) D.C. source
v(t)E
II) Time variant sources :
The sources in which voltage is varying with time are known as time variant voltage sources or A.C. sources. These are denoted by small letters. This is shown in the Fig. 1.6 (b).
Flg. 1.6 (b) A.C. source
1.4.2 Current Source Ideal current source is the source which gives constant current at its terminals irresp ective of the voltage appearing across its terminals. The symbol for ideal current source is shown in the Fig. 1.7 (a). This is connected to the load as shown in the Fig. 1.7 (b). At any time, the value of the current flowing through load IL is same i.e. is im.'Spective of voltage appearing across its terminals. This is explained by V-I characteristics shown in the Fig. 1.7 (c). tl
IL +
'·
.
~
Land
vl
'·
ll = '•
VL
0 (a) Symbol
(b) Circuit
Fig. 1.7 Ideal
cum~nt
(c) Char• ctorlstles
source
Copynghtcd materia
Circuit Theory
1 -6
Basic Circuit Analysis & Network Reduction Techniques
But practically, every current source has high internal resistance, shown in parallel with current source and it is represented by R,h. This is shown in the Flg. 1.8. It
._,,,~~o
Thus as 1., Increase, IL.
decteases , .l l < '·
0 '-------~ IL (b) Characterladc
(a) Circuit
Fig. 1.8 Practlcal current source
Because of R.-, current through its terminals decreases slightly with increase in voltage a t its terminals. Key Point : For ideo/ current source, R51, = -. Si.rnilar to voltage sources, current sources arc classified as follows : I) Time invariant sources :
The sources in which current is not varying with time arc known as time invariant current sources or D.C. sources. These are denoted by capital letters. Fig. 1.9 (a) D.C. source
Such a current source is represented in the Fig. 1.9 (a).
ii) Time variant sources :
The sources in which current is varying with time are known as time variant current sources or A.C. sources. These are denoted by small letters. Fig. 1.9 (b) A.C. source
Such a Fig. 1.9 (b).
source
is
represented
in
the
The sources which are discussed above are independent sources because these sources does not depend on other voltages or currents in the network for their value. These are represented by a circle with a polarity of voltage or direction of current indicated inside.
1.4.3 Dependent Sources Dependent sources are those whose value of source depends on voltage or current in the circuit. Such sources are indicated by diamond as shown in the Fig. 1.10 and further classified as,
Copynghl"
1·7
Circuit Theory
Basic Circuit Analysis & Networ* Reduction Techniques
I) Voltage dependent voltage s ource : It produces a voltage as a function of voltages elsewhere in the given circuit. This is called VDVS. 11 is shown in the Fig. 1.10 (a). ii) Current dependent current source : 11 produces a current as a function of currents elsewhere in the given circuit. This is called CDCS. It is shown in the Fig. 1.10 (b). iii) Current dependent voltage source : It produces a voltage as a function of current elsewhere in the given circuit. This is called CDVS. It is shown in the Fig. 1.10 (c).
lv) Voltage dependent current source : It produces a current as a function of voltage elo;ewhere :n the given circuit. This is called VDCS. It is shown in the Fig. 1.10 (d).
V·K·,c I=KV,E
(o)
(d)
(e)
(b)
Fig. 1.10 Types of dependent sources K is constant and \\ and 11 arc the voltage and current respectively, present elsewhere in the given circuit. The dependent sources are also known as controlled sources.
1.4.4 Regulation and Loading of Sources It is seen that practically the output voltage of the voltage source decreases as load current increases. The allowable drop in voltage is specified in of parameter called
regulation of source. It is defined as, ., .l . No load ''oltage-Fullload voltage VNt. - VFL % r..egu ation = x 100 = x 100
Full load voltage
VFL
On no load, VNL is same as the rated value of voltage source. While VFL is terminal voltage on full load. Key Point : Lesser lk regulation, beller is I~ perforiii/Jtu:e of lire source. Ideal 'CI
said to be loaded. This is loading of sources. +
Hl
For example : Consider the source of 10 V shown having internal resistance of l!l, in the Fig.1.11. The terminal voltage is,
v, ... (J)
Ag. 1.11 Loaded source
Circuit Theory
1-8
Basic Circuit Analysis & Network Reduction Techniques
On no load, Rt =~and Vo = V=VNt = 10 V
let the specified full load current be 1 A i.e. IL =I ft. =1 A. On full load,
10 .Rt. = - - 1=9n IL
... from (1)
= IFt.XRt =1x9= 9V % Rcgu.lation
= VNL - VFL x100 = l0 - 9 xt00 = 11 .11% VFL 9
If now Rt. is changed to sn then,
vl
10 It. = S+ 1 = 1.667 A
Allowable
value I
VNI.~-..;.;-:.::-- +--------Ideal
. . loading
ot source
Fig. 1.12 Loading of source
..
VL = It Rt = 1.667x5 = 8.335 V
:.'Yo Regulation=
;~~5 x100 = 19.97%
10
1his worsens the regulation and the source i.q said to be loaded. Thus for any I L > 1 A there is loading of source which Is shown in the Fig. 1.12.
1.5 Ohm's Law This law gives relationship between the potential difference (V), the current (I) and the resistance (R) of a d.c. circuit. Dr. Ohm in 1827 discovered a law called Ohm's Law. It states,
Ohm's Law : The currtnt flowing through the eltetric circuit is directly proportionRI to the pottntial differtnce Rcross the circuit Rnd invmtly proportim14/ to tire reslstRnce of tire circuit, provitkd the temptrQiurt remoins constant.
Mathematically, +
R
'\'-~VI/VI,-"'/ v Fig. 1.13 Ohm's law
Where I is the current Oowing in amperes, the V is the voltage applied and R is the resistance of the conductor, a.q shown in the Pig. 1.13.
v
Now I= R
The unit of potential difference is defined in such a way that the constant of proportionality is unity.
Copyrgh!cd malcri~
Circuit Theory
1-9
Basic Circuit Analysis & Network Reduction Techniques
amperes
Ohm's law is,
volts
V =I R
Tv
= Constant = R ohms
The Ohm's law can be defmed as, The ratio of potential difference (V) between any two points of a conductor to the current {I) flowing between them is constant, provided that the temperature of the conductor remains constant.
Key Point: Olrm's ltnu can be applied tithn to tire aalire circuiJ or to the part of a circuit.
If it is applied to entire circuiJ, tire voltage across 1M entire circuit and resistance of tire entire circuit slrould be taken into . If tire Ohm's ltnu is applied to tire part of a circuit, then tire resistance of tluzt part and potential across tlrat part should be used.
1.5.1 Limitations of Ohm's Law The limitations of the Ohm's law are, 1) It is not applicable to the nonlinear devices such as cliodes, zener cliodcs, voltage
regulators etc. 2) It does not hold good for non-metallic conductors such as silicon carbide. The law
for such conductors is given by, V = k Im
where k, m are consY.nts.
1.6 Linear ive Parameters (R, L and C) The three basic linear ive elements used In various circuits are, 1) Resistance
2) Inductance
3) Capacitance
1.6.1 Resistance and Its V-1 Relationship R
o----'IVMr----<>o +
v -
Fig. 1.14
It is the property of the material by which It opposes the flow of current through it The resistance of element is denoted by the symbol 'R'. Resistance is measured In ohms (0). The relation between voltage and cu:rrcnt is given by Ohm's Jaw.
V = R·l
Copynghtcd materia
Circuit Theory
1 • 10
Baste Circuit Analysis & Network Reduction Techniques
Resistor dissipates energy in the form of heat. So power absorbed by the ~istor is given by,
IP
= VI = (I R) I
2
%
1R =
~ watts I
Resistance converts amount of energy into heat during time I, is given by, I
W = Pdt = Jt2 Rdt = t2 · R·t =V · I · t
joules
0
1.6.2 Inductance and its V·l Relationship Inductance is the element in which energy is stored in the form of electromagnetic field. The inductance Is denoted by 'L' and it is measured in Henry (H).
L
o-o--'WO"G'~--oo
• v -
For inductance, the voltage is proportional to the rate of change of cunt'nt.
Fig. 1.15 :. v
«
di dt = L di(t)
dt Assuming that initially zero current flows through the inductance, if a current i is made to flow through a coil, the energy stored in time interval is given by, I
W = J vidt 0
W =
1
2
d. )
I (
I
= J Ld: idt
= LJi·di (I
(I
i2L joules
... Energy stored in an inductor.
1.6.3 Capacitance and its V-1 Relationship + 0
v(t) - 0
lc T
Fig. 1.16
An clement in which energy is stored in the form of electrostatic field is known as capacitance. The capacitance is denoted by 'C' and it is measured in Farads (F). For capacitor, the voltage is proportional to the charge.
..
v
«
q
Copyrgh!cd malcri~
Circuit Theory
1 • 11
Basic Circuit Analysis & Network Reducction Techniques l
v
0(
v = i
Jidt
~Jidt
= C dv(t) dt
With zero inJtial voltage across capacitor, if the current I flows for time t spent, the energy supplied to capacitor will be, l l dv v W = J v.idt = v. Cdtdt = C vdv 0
J
J
0
0
... Energy stored in a capacitor.· Key Point : While CAlculating energy stared in the t:apQcitar, V must be voltage across
capacitor. Summarizing the behaviour of the three basic elements, we can write, Element
Voltage across element If current Ia known
R
v • iR
l
v • l dt
Current through element If voltage Is known
dl
c
v•
~Jidc
v
i
•R
i
m
f[vdl
I=C~
Table 1.1 Behaviour of circuit elements ,,.. Example 1.1 A 0.5
Ill' C11pQcitar has volt4ge llJtt'/Hform
v(t)
(Fig. 1.17) .Plot i(l) as
function of I .
•(Aprl~·2005)
v(t)
2
4
8
t (msec)
Fig. 1.17
Copyngh!cd materia
Circuit Theory
1 • 12
Basic Circuit Analysis & Networfl Reduction Techniques
------~--------------
Solution : For 0 < t < 2, v(t) is a ramp of slope
~ = 20. ... for0
<2
v(t) = 20 t i(t) For 2 < t < 4, v(t) is
= Cdd~l)
=0.5x 10-6 x20 =1xt0·5A= lOI!A
... for0
<2
con.~tant.
v(t) = 40 V
... for2
<4
dv(t) _ -6 i(t) = Cdt = O.::>XlO xO = 0 A
... for2
<4
For 4 < t < 8, v(t) is a ramp with slope =
0 ~~ = - 10 8
v(t) = -10 t + 80
... for4
<8
i(t) = C d~~t) = 0.5x t0-6 x(-10) =- 5 IJ.A.
... for4<1<8
The current waveform is shown in the Fig. 1.17(a). ~I)
10~A I---.
Fig. 1.17(a) NutP. : For 4 < t < 8 , the equation of the line is y = mt + C where m = slope = -10. It gives equation y = - 10 t + C. Now point (8, 0) is on the line so substituting in the equation,
0 = -10x8+C
i.e. C = 80
Thus equation of line is y = - 10 t + 80 where y = i(t), as used above.
1.7 Analysis of Series Circuits A series circuit is one in which several resistances are connected one after the other. Such connection is also called end to end connection or cascade connection. There is only one path for the flow of current. Copyrgh!ed matcri~
Circuit Theory
1 ·13
Basic Circuit Analysis & Network Reduction Techniques
1.7.1 Resistors In Series Consider the resistances shown in the Fig. 1.18.
....._ R2
•
.I.
.I.
?-- V,---t-- v2
.:II.
•
~.(!.
I
v3-•
-
Vvolts
Fig. 1.18 A series circuit
The resistance R 1 , R 2 and R3 are said to be in series.. The combination is connected across a source of voltage V volts. Naturally the current flowing through all of them is same indicated as I amperes. e.g. the chain of small lights, used for the decoration purposes is good example of series combination.
Now let us study the voltage distribution. Let v,, V2 and V3 be the voltages across the terminals of resistances R1, R2 and R3 respectively.
v
Then, Now accord ing to Ohm's law,
=
v 1 + v2
+
v3
V1 = IR 1 , V2 =IR2 , V 3 = 1 R 3
Current through aU of them is same i.e. I
Applying Ohm's law to overall circuit, V = I Rc'
Rcq = R1+R2 +R3 i.e. total or equ ivalent resistance of the series circuit is arithmetic sum of the resistances connected in series. For n resistances in series,
1.7.1.1 Characteristics of Series Circuits 1) The same current flows through each resistance. 2) The supply voltage V is the sum of the individual voltage drops across the resistances. V = Vt + V2 +..... + Vn
Copyrgh!cd malcri~
1 • 14
Circuit Theory
Basic Circuit Analysis & Network Reduction Techniques
3) The eqwvalcnt resistance is equal to the sum of the individual l'eSistances. 4) The equivalent resistance is the largest of all the individual resistances.
i.e
1.7.2 Inductors in Series Consider the Fig. 1.19 (a). Two inductors L 1 and L.2 are coMe<:ted in series. The cunents flowing through l. 1 and l.z nre i 1 and iz while voltages developed across L 1 and L 2 nrc Vl t and VL2 respectively. The cqlrivalcnt circuit is shown in the Fig. 1.19 (b).
vL • o-o--~'----oo Leo (b)
(a)
Fig. 1.19 Inductors in series
di
VL = Lcqdt
We have,
For series combination,
and
Yt
~
Vu • Yt.z
..
di di di Lcq - = Lt Ji + Lz dt dt
..
L
di
cq
..
di dl = (Lt + L,• )ift
L,"
~
Lt + L2
That means. equivalent inductance of the series combination of two ;nductances is the · sum oi inductances coMccted in series. Key Point : The total equivalent inductance of the series circuit is sum of the inductances connected in series.
For n inductances in series,
l.
L,q =
1-t+~+~+ ... +t.,
Copyrgh!cd malcri~
Circuit Theory
Basic Circuit Analysis & Networ11 Reduction Techniques
1 • 15
1.7.3 Capacitors in Series Consider the Fig. 1.20 (a). Two capacitors C1 ;md C2 arc connected in series. The currents flowing through and voltages developed across C1 and C2 are i 1, i 2 and Vc 1 and Vcz respectively. The equivalent circuit is shown in the Fig. 1.20 (b).
•
Vel
·w cl
il
vc
Vc2
12
' ·~~-
i
• ' y
•
~
•
ci!Q
(a)
(b)
Fig. 1.20 Capacitors In series I
We have,
Vcz =
c2
For se.ries combina lion, i
~
i1
~
Vc
~
Vc 1 + Vcz
iz
I
Ji 2
--
d1
while
I V = Ceq
I .
J1d1
--
and
I
-c cq
Jidt -~
= it = i2
But I
I )' Jidl J idt = ( -+ C1I -Cz __ Ceq I
Ceq
Ceq
I
= -+-
c, c2
= c1c1c2 +C2
That means, reciprocal of equivalent capacitor of the series combination is the sum of the reciprocal of individual capacitances.
Key Point : Tlu rtciproall of the total equivalent CJJPIIcitor of tlu series combination is tht sum of 1/u rtciproco/s of the individual azpacilors, connected in str~. For n capacitors in series,
Copyngh!cd materia
Circ:uit Theory
to+
1 -16
Basic: Circuit Analysis & Networt Reduc:tion Tec:hniques
Example 1.2 : Twv o:apacittmctS C 1 and C2 of values of ~0 p.F and 5 p.F, respectivtly are comzccted in series. What is tile equivaltmt capacitance of lht combination ? [Aprii/May-20031
Solution :
C 1 = 10 11F
Ceq = ..
and
Cz = Sj1F
C 1C 7 = lOx 10· 6 xSxlO - 6 = 3 .333 x 10 _ 6 Ct +C2 lOx 10-6 +Sx to- 6
= 3.33 )IF
1.8 Analysis of Parallel Circuits The parallel circuit is one in which several resistances a.rc connected across one another in such a way that one terminal of each is connected to form a junction point while the remaining ends are also ed to form another junction point.
1.B.1 Resistors in Parallel Consider a parallel cil'cuit shown in the Fig. 1.21. In the parallel connection shown, the three resistances R 1 , R 2 and R 3 are connected in parallel and combination is connected across a source of voltage 'V ',
R, • v ~
In parallel circuit current ing through each resistance is different. Let total current drawn is say ' I ' as shown. There are 3 paths for thi• current, one + v through Rt, second through R2 and third through R3. Depending upon the values of R, , Rz and R3 the + appropriate fraction of total current es through v them. These individual currents are shown as I t ,lz and Fig. 1.21 A para.l lel c:irc:uit I 3· While the voltage across the two ends of each resistances R1 , R2 and R3 is the same and equals the supply voltage V. +
v -
Now let us study current distribution. Apply Ohm's Jaw to each resistance. V = 11 R 1 , V = 12 R2 , V = 13R 3 11 =
v R;"'
v
v
12 = Rz ' 13 = R3
v
v
v
= 11 +12 +13 = - + - + Rt Rz R3 ... (1)
For overall circuit if Ohm's Jaw is applied, V = I Req
Copyrghtcd malcri~
Circuit Theory
1 - 17
and
Basic Circuit Analysis & Networlt Reduction Techniques
I=Rv
... (2)
eq
Rcq = Total or
Where
equiv~lent
rHistance of the circuli
Comparing the two equations, 1
1
1
1
- - = - +- + Rt R2 R3 Rcq Where R is the equivn.lcnt
resista~
of the pa.rallel combination.
In general if 'n' resistances are connected in p arallel, 1
R
1 I 1 1 = Rl+ R2 + R3 +......+ Rn
Conductance (G) : It is known that,
I
1 R =
G
(conductance) hence,
G = G t +G2 +G3+......+Gn
... For parallel drcult.
Important result : Now if n = 2, two resistances are in parallel then,
1
R
1 Rt
1 R2
= - +-
R = This formula is directly used herea fter, for two resistances in parallel. 1.8.1.1 Characteristics of Parallel Circuits I) The same potential difference gets across aU the resistances in parallel. 2) The total current gets divided into the number of paths equal to the number of
resistances in parallel. The total current is always sum of all the individual current~.
I = It +l2 + I J +.. ....+ln 3) The redprocal of the equivalent resistance of a parallel drcuit is. equal to the sum of the redprocal of the individual resistances.
4) The equivalent resistance is the smallest of all the resistances.
R < Rt , R
Circuit Theory
1 · 18
Basic Circuit Analysis & Network Reduction Techniques
5) The equivalent ::onductancc is the aritlunctic addition of the individual conductances. Key Point : Th~ equiwltnt resistance is sma//er than lite smallest of a// the rtsistances connt'cled in para/lei.
1.8.2 Inductors In Parallel Consider the Fig. 1.22 (a). Two inductors L 1 and L 2 are connected in parallel. The currents flowing through L1 and L 2 are i 1 and i 2 respectively. The voltage developed across L1 and L2 are VL 1 and VL2 respectively. The equivalent circuit is shown in Fig. 1.22 (b). ;, +
o-o--<-~---oo
Leq
lz
{b)
(a)
Fig. 1.22 Inductors In parallel
For inductor we have,
r.I JVLI d1,
t
t
i1 ;
L2
- ~
JV1.2 dt,
while
.
I
I = -
-~
Leq
t
--
jVLd t
For parallel combination, VL = VLI = VL2
= il + L,-q
J' V..dt
--
Lcq
and
jl I
= =
I
I JvLdt - I J VLdt + l.o L2
--
(I
' = L.+i2I )_J_vL dt
-w
I I -+ -
L,
t2
That means, reciprocal of L'<juivalent inductance of the parallel combination of reciprocals of the individual inductances.
i~
the sum
For n inductances in parallel, I
Lcq =
1
I
I
I;'+ l2 +....L;
Copyrghlcd malcri~
Circuit Theory
1 ·19
Basic Circuit Analysis & Network Reduction Techniques
1.8.3 Capacitors In Parallel Consider the Fig. 1.23 (a). Two capacitors C1 and C1 are connected in parallel. The currents flowing through C1 and C2 are i 1 and i 2 respectively and voltages developed across c,, C2 are Vel and Vc2 respectively. The equivalent circuit is shown in the Fig. 1.23 (b).
c,
Vc
....-~·u c..,
•
Cz (a)
(b)
Fig. 1.23 Capacitors in parallel
1=
For capacitor w e have,
ccqdt dVc
For parallel combination, Vc 1 "
Vc2 " Vc
and
= i, + i2
c
..
..
dVc
dVc, c dVc2 = c 'd!+ ld(
dVc
dt = ('c, + c2 )dYe
"'ld!
c
"'ld!
C.:q =
c, + c2
That means, equivalent capacitance of the parallel combination of the capacitances is the sum of the individual capacitances connected in series. For n capacitors in parallel,
Copyrghtcd matcri~
Ci rcuit Theory
1 - 20
Basic Circuit Analysis & Networll Reduction Techniques
The Table 1.2 gives the equivalent at 'n' basic elements is series. Element
Equival ent.
·n• Resistances in series
R, R , R,
R •
· ·· - ~
....
Req = R1 + R2 • R3 + ... + R,
'n' lnductOts 1n series L,
L,
L,
· · ·-~ l•
....
Leq = L1 + L2 + L3 + ... + ln
'n' Capacitors in series
o-ll c,
0
II
0
c,
11--.... o-ll--
c,
c.
1
I
t
t
= - + - + ···+Ceq Ct C2 Cn
Table 1.2 Series combinations of elements
The Table 1.3 gives the equivalent of 'n' basic elements in parallel. Element
Equivalent
'n' Resistances in parallel
~:~r~r~:JR.
1 -
Req
Q
1 1 1 - + - + ·-·+ R1 R2 Rn
'n' Inductors In parallel
~=r~~r~=J·
t
1
1
1
-l cq = -l 1 + -L2 +·-·+Ln-
'n' Capacitors in parallel
c.I __ , 1 c., c,f I __ . J c.
0
Ceq
=C1 + C2 + ...+ Cn
0
Table 1.3 Parallel combinations of elements
Copyngh!cd materia
Circuit Theory
1 -21
Basic Circuit Analysis & Network Reduction Technlquas
Key Point : Tht currtnt through strits combination remains same and voltage gets dillidtd
I..
while in parallel combitwlion voltage across combination remains same and current gets divided. Example 1.3 : Find the equivaltnt resistance between the two paints A and B shown in
the Fig. 1.24. 30
....A. A. AA
40
.?.R
4{l
10 A
6!1
50
B
Hl
Fig. 1.24 Solution : Identify combinations of series and parallel resistances.
The resistances 5 n and 6 n are in series, as going to So equivalent resistance is 5
carry same current.
+ 6 = 11 n
While the resistances 3 n , 4 n, and 4 n are in parallel, as voltage across them same but current divid es. :. Equivalent resistance is,
R = 3 +4+4 =i2
1
1
1 1
10
..
R =
12 iii = 1.2n
Replacing these combination.< redraw the figure as shown in the Fig. 1.25 (a). 20
Series 1.2 0
ParaUel
10 A
Fig. 1.25 (a)
Fig. 1.25 (b)
Now again 2.2 n and 2 n are in series so equivalent resistance is 2 + 1.2 = 3.2 n while 11 n and 7 n are in parallel. 77 Using formula ~t+Ri equivalent resistance is ~~:; = 18 =4.2770.
2
Copyrghtcd matcri~
Circuit Theory
1 - 22
Basic Circuit Analysis & Network Reduction Techniques
Replacing the respective combinations redraw the circuit as shown in the Fig. 1.25 (b). Now 3.2 and 4.277 arc in parallel. 3 . 2x 4.277 3 .2+4 .277
Replacing them by
~
1.8304
n
RAB. ~ 1+ 1.8304 ~ 2.8304 0
1.9 Short and Open Circuits In the n etwork simplification, short circuit or open circuit existing in the network plays an important role.
1.9.1 Short Circuit
.------
'•a
When any two points in a network are ed directly to e:ach other with a thick metalic conductin,g wire, the two points are said to be short circuited. The resistance of such short drcuil is zero.
,
A ~----~~.---1
Thiel< conducting -
Netwod<
wire a~---....1.--<
·'------
The part of the network, which is short circuited is shown in the Fig. 1.26. The points A and B are short circuited.
Fig. 1.26 Short circuli
The resistance of th e branch AB is R.., = 0 0 . The curent JAB is flowing through the short circuited path. According to Ohm's law, VAB
=
R.., X lAB
= 0 X lAB = 0 V
Key Point : 'flrus, voltage across slrort circuit is always zero though cu.rrent f/17WS througlr
the short circuited patlr.
1.9.2 Open Circuit When there is no connection between the two points of a network, having some voltage across the two points then the two points are said to be open circuited. A+
t
Open
circuit
R,
T.o
l ~___ B-
: - - - - --
:
R t 2 :
.__.....:
Netwol1!
' L------
Fig. 1.27 Open c ircuit
As there is n o direct <:onneclion in an open circuit, the resistan ce o f the op en circuit is oo.
The part of the network which is open circuited is shown in the Fig. 1.27. The points A and B arc said to be open circuited. The resistance of the branch A B is Roc ="" 0.
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Circuit Theory
1 -23
Basic Circuit Analysis & Network Reduction Techniques
There exists a voltage across the points AB called open circuit voltage, VAB but
Roc=- 0. According to Ohm's law, loc
= VAs =VAs =0 A Roc oo
Key Point : Thus, currtnt through open circuit is always uro thuugh there exists a voltage
across
optn
circuited terminals.
1.9.3 Redundant Branches and Combinations The redundant means excessive and unwanted.
Key Point : If in a circuit there are bra11dres or combinations of tlements which do not carry any curre11t thtn such bra11ches and combinations an! called redundant from circuit point of view. The redundant branches and combinations can be removed and these branches do not affect the performance of the circuit The two important situations of redundancy which may exist in practical circuits are, Situation 1 : Any branch or combination across which there exists. a short circuit, becomes redundant as it does not carry any current.
U in a network, there exists a direct short circuit across a resistance or the combination of resistances then that resistance or the entire combination of resistances becomes inactive from the circuit point of view. Such a combination is redundant from circuit point of view. To understand this, consider the combination of resistances and a short circuit as shown in the Fig. 1.28 (a) and (b).
·~ ~ (a)
-.
R2
I
Short
•
vc ~
-
A
~ 1=0
R;, R,
R.. ;
No current through R3
*I
:\
B
\
Short
No current
through R3 and R4
(b)
Fig. 1.28 Redundant branches
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Circuit Theory
Basic Circuit Analysis & Network Reduction Techniques
1 - 24
In Fig. 1.28 (a), there is short circuit across R3. The current always prefers low resistance path hence entire curr~'llt I es through short circuit and hence resistance R3 becomes redundant from the circuit point of view. In Fig. 1.28 (b), there is short circuit across combination of R3 and R4. The entire current flows through short circuit across R3 and and no current can flow through combination of ~ and ~· Thus that combination becomes meaningless from the circuit point of view. Such combinatioJU can be eliminated while analysing t:he circuit.
a.
Situation 2 : U there is open circuit in a branch or combination, it can not carry any current and becomes redundant. In Fig. 1.28(c) as there exists open circuit in branch BC, the branch llC and CD can not carry any current and are become redundant from circuit point of view. ~Redundant
R,
A
B
~
c
!
I%0
Rz
I)
R4
1=0 E
F
ranches
D
Fig. 1.28(c) Redundant branches due to open circuit
1.10 Voltage Division In Series Circuit of Resistors Consider a series circuit of two resistors R 1 and R2 connected to SO\liCe of V volts. As two resistors are connected in series, the
current flowing through both the resistors is same, i.e. L Then applying KVL, we get, V = I Rt +I R2
v
Fig. 1.29
:. I= Rr + R2
Total voltage applied is equal to the
sum
of voltage drops
VRr
and
VR2
across Rt and
R2 respectively.
..
..
VRI
= I. Rt
VRI =
Similarly,
VRl
V
Rt + R2
·Rt = [
RI ] V Rt + R2
= I· R2
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Basic Cin:uit Analysis & Network Red uc tion Techniques
1 - 25
Circ:uit Theory
So this circuit is a voltage divider drroil Key Point : So in general, voltage drop llCI'OSS any resistor, or combination
of resistors, in a series circuit is equal to the ratio of that resistance value to the total resistance, multiplied by the source voltage.
1.11 Current Division in Parallel Circuit of Resistors Consider a parallel circuit of two resistors R1 and Rz connected across a source of V volts. Current through R 1 is l1 and Rz is l2, while total current drawn from source is h.
.. But i.e.
Fig. 1.30
'• = lz
.,. =
'• + lz
v
'• =
~,
12 =
v
Ri
V= IIRI = lz Rz
(~~ )
Substituting value of 11 in I,., IT = lz (
lz =
Now
•• ••
~~ ) + l2
= 12
[~~ +1]
= 12 [ R• : R2] 1
[R.~RJ ,,.
= ,,. - 12 =
,,. - [ R1R1+R2 ] ,,.
1 2 1 = [R +R -R ] IT
'• = [
Rt +Rz
R,- ] .,. R1 +R2
Key Point : lr1 general, the current in any branch is equal to tloe ratio of opposite branch resista11ce to the total resistance VQ/ue, multiplied by the total current in tl1e circuit.
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Circuit Theory
••
1 • 26
Basic: Circ:ult Analysis & Network Reduction Techniques
Example 1.4 : Find the voltage across tht three resistances shown in lltt Fig. !.3!.
100
200
300
(' + -
60V
Fig. 1.31 Solution :
=
v
... Series circuit
Rt +R2 + R3
60 = 10+20+ 30 = lA VRI = !RI =
VxRt = l xlO = 10 V Rt +Rz +R3
VxR 2 = lx20=20V VR2 = I R, = • R t +Rz +R J
and
VRJ = IR J =
VxR3 =l x30 = 30 V Rt +Rz + R3
Key Point : II can be seen that voltage across any resistanc~ of series circuit is ratio of that
resistance to the total resistance, multiplied by the source voltage. ••
Example 1.5 : Find the magnitudes of total CIITrtnt, current through R 1 and R 2
Rt= 10 Q, Rz= 20
Q,
if.
and V= 50 V.
t
•• R, : Fig. 1.32
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Circuit Theory
1 • 27
Basic Circuit Analysis & Network Reduc tion Techniques
Solution : The equivalent resistance of two is,
v lr = -Rcq
50 = -- =
6.67
7.5 A
As per the current distribution in parallel circuit,
Il = = and
12 =
lr( RI~R2 )= 7
sx( 10~20)
SA
lr( RI~IR2 )= 7 .5x( 10~20)
= 2.SA It can be verified that
1.12 Source Transfonnation Con.
if Ill~ supply equal load current to
tire load, with sa= Wad connectd llCTOSS its terminals The current delivered in above case by voltage source is,
Rsc and R L in series
.. . (1)
If it is to be replaced by a current so= then load
current must be (
v
. )
Rsc +RL
Consider an equivalent current sowce shown in the Fig. 1.33 (b). Fig. 1.33 (b) Current source
The total current is · I ·.
Both the resistances will take current proportional to their values.
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Cln:ult Theory
Bask: Cln:ult Analysis & Network Reduction Teehn.Jqua
1 • 28
From the current division in paraUel circuit we can wrile,
1L = !>< Now this IL and R
.,R
.:..R~sb~"7
must be same, so equating (1) and (2),
sc + L
v
= R.., = R,h = R say.
Let internal resistance be,
v =
Then,
1
or
..
=
1=
Key Point :
.•.(2)
(Rob +RL)
I>< Rsb
= I>< R
v Rsh
v R
=
v Rse
If wltAge source is converted to current source,
thnt CUI'Tent source I = - v
R,..
with parallel irrtmu1l resistAnce el(UIII to R". Key Point :
with series
If currtnt source i.< converted to voltage source, tllm voltage source V = I R.I.
intmu~l
resistance equal to R.h.
The direction of current of equivalent current source is always from Internal to the source. While converting current source to voltage source, voltage is always as +ve terminal at top of arrow and -ve temtinal at bottom direction of current is from -ve to +ve, internal to the source. This ensures flows from r
ve to + ve, polarities of of arrow, as that current
Note the directions of transformed sources, shown in the Fig. 1.34 (a), (b), (c) and (d) .
• :::: I
(a)
I-~ Rae
(b) I • -
v
R..
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Clreult l'Mory
Basic: Cireuit Analysis & Network Reduc:tlon Tec:hnlqun
1 • 29
R,.
-
v
(c:) V • l x R ah
(d) V • I XRst>
Fig. 1.34 Sourc:e transfonnatlon ,_,. Example 1.6 :
Transform a voltage sour~
of 20 volts
with an inttnUJi rtsist;Jnct of 5 0
to 11 current source. Solution: Refer to the Fig. 1.35 (a). 50
50
(b)
(a)
Fig. 1.35 Then current of curren t source is, I
=
R: = ;o =
4 A with internal p arallel resistance
same as R"' . :. Equivalent current source is as shown in the Pig. 1.35 (b).
'' *
Example 1.7 :
1April!May·20041
Convert into a w/tage source.
10A
t
50
Fig. 1.36
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Circuit Theory
1 • 30
Bailie Circuit Analysis & Network Reduction Techniques
so
Solution :
I = 10 A,
v
= IX R
R = 5 !l
~
10 X 5 = 50
v
The polarities are positive at top and negative at bottom of the anow. Thus the voltage source is as shown in the Fig. 1.37.
Fig. 1.37
1.13 Combinations of Sources In a network consisting of many sources, series and parallel combinations of sources exist. II such combinations Me replaced by the equivalent source then the· network simplification becomes much more easy. Let IL~ consid er such series and parallel combinations of energy sources.
1.13.1 Voltage Sources In Series If two voltage sources are in series then the equivalent is dependent on the polarities
of the two sources. Consider the two sources as shown in the Fig. 1.38.
Fig. 1.38 (1.1) Thus ;J the polarities of the two sources arc same then the equivalent single source is the ~ddition of the two sources with polarities same as that of the two sources. (a)
Consider the two sources as shown in the Fig. 1.39.
(a)
Fig. 1.39
(b)
Thus if the polarities of the two sources are different then the equivalent single source is the difference between the two voltage sources. The polarities of such source is same as that of the greater of the two sources.
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Circuit Theory
1 • 31
Basic Circuit Analysis & Network Reduction Techniques
Key Point : The voltage sources to be connected in series must have s.ame current ratings
though thrir voltage ratings may be same or different. The technique can be used to reduce the series combination of more than two voltage sources connected in series.
1.13.2 Voltage Sources in Parallel Consider the two voltage .sources in parallel as shown in the Fig. 1.40.
v, •
The equivalent single source has a value same as V 1 and V 2. It must be noted that at the terminals open circuit voltage provided by each source must be equal as the sources are in parall2l.
Fig. 1.40
Key Point : Heuce the voltage sources to be connected in paratltl rrurst IUW
1.13.3 Current Sources in Series Consider the two current sources in series as shown in the Fig. 1.41. The equivalent single source has a value same as 11 and 12.
Key Point : The current through series circuit is always same hence it must be noted that the current sources to be connected in series must have same current ratings though 1/reir voltage ratings may be same or different.
Fig. 1.41
1.13.4 Current Sources In Parallel Consider the two current sources in parallel as shown in the Fig. 1.42.
=::;
(a)
Fig. 1.42
(b)
Thus if the directions of the currents of the sources connected in parallel are same then the equivalent single source is the addition of the tWo sources with direction same as that of the two sources.
Circuit Theory
1 • 32
Basic Circuit Analysis & Network Reduction Techniques
~----------------~------------------~ Consider the two current $0Urces with opposite directions connected in parallel as
shown in the Fig. 1.43.
(a)
(b)
Fig. 1.43
Thus if the directions of the two $0urces are different then the equivalent single source has a direction same as greater of the two soun:es with a value equal to the difference between the two sources. Key Point : Tire cu"o't S()urces to be conntcled in parallel must l!lzw same ooiU!ge ratings though thtir cumnt ratings may be same or diff~ent.
1.14 Kirchhoff's Laws In 1847, a German physicist, Kirchhoff, formulated two fundamental laws of electricity. These laws are of tremendous importance from network simplification point of view.
1.14.1 Kirchhoff's Current Law (KCL) Consider a junction point in a oomplex network as shown in the Fig. 1.44. At this junction point if It= 2 A, l 2 = 4 A and !3 = 1 A then to determine 14 we write, total current entering is 2 + 4 = 6 A while total current leaving is 1+ 14 A Fig. 1.44 Junction point
And hence,
14 = 5 A.
This analysis of currents entering and leaving is nothing but the application of J
Another way to state the law is,
Tlu algebraic 61lm of all the currmt meeting 11t a junction point Is always zero. The word algebraic ~)
meaN
considering the signs of various cuJTents.
at junction point = 0
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Circuit Theory
1 - 33
Basic Circuit Analysis & Network Reduction Techniques
Sign convention Currmts flowing towards a jlmction point .are .auum~ to be positive while currm ts flowing away from a jumtion point ass~ to be negative. e.g. Refer to Fig. 1.44, currents !1 and !2 arc positive while l 3 and l4 arc negative. Applying KCL,
L I at junction 0
= 0
l1 +l 2 -J3 - 14 = 0 i.e. l1 +l2 = l3 +l4
The law is very helpful in network simplification.
1.14.2 Kirchhoff's Voltage Law (KVL) "In IUf'!/ network, the algebraic sum of the voltage drops across the circuit elemmts of any clo~ p.ath (or loop or mesh) Is equal to thl! algebraic sum of the e.mfs in the path" In other words, ''the algebraic sum of all the branch voltages, around any closed path or closed loop is always zero."
I
Around a closed path
R
R
Ao---J\II/IIIr--8 -
L V= 0
A o---J\II/IIIr--8
+
-I
+ 1-
The law states that if one starts at
a
goes on tracing and noting aU the potential changes
certain point of a closed path and
(either drops or rises), in any one particular direction, till the starting point is reached again, he must be at the same potential with which he started tracing a closed path. (a)
Fig. 1.45
(b)
Sum of aU the potential rises must be equal to sum of all the potential drops while tracing any closed path of the circuit. The total change in potential along a closed path is always zero.
nus law
is very useful in the loop analysis of the network.
1.14.3 Sign Conventions to be Followed while Applying KVL When current flows through a resistance, the voltage drop occurs across the resistance. The polarity of this voltage drop always depends on direction of the cu:rrcnt The current
always flows from higher potential to lower potential. In the Fig. 1.45 (a), current I is flowing from right to left hence point B is at higher potential than point A, as shown. In the Fig. 1.45 (b), current I is flowing from left to right, hence point A is at higher potential than point B, as shown.
Once all such polarities are marked in the given circuit, we can apply KYL to any closed path in the circuit. Now while tracing a closed path, if we go from - vc marked tcrmirull to + ve marked terminal, that voltage must be taken as positive. This is called potential rise.
Copyrghtcd malcri~
Ci~~ Theo~ ~------1_-_34 __-=B~as~i~c~C~Ir~c~ui~t~Ana~l~y~al~a~&_N_e_hNG ___~__ Red -=u~c~ti~ ·o~n_T~ech -=n_l~q-uea __ For example, If the bronch AB is traced from A to B then the drop across it must be considered as rise and must be taken as + I R while writing the equations. While tracing a closed path, if we go from +ve marked tertnin:al to - ve marked terminal, that voltage must be taken as negative. This is called potential drop. For example, in the Fig. 1.45 (a) only, if the branch is traced from B to A then it should be taken as negative, as - I R while writing the equations. Similarly in the Fig. 1.45 (b), if branch is traced from A to B then there is a voltage drop and term must be written negative as - I R while writing the equation. If the branch is traced from ll ! tl A, it becomes a rise in voltage and term must be written positive as + I R while writing the equation.
Key Point : 1) Potential rist i.e. travelling from negative to positively marked ltrmina/, must ~ considaed as Positivt. 2) Potential drop i.e. travelling from positiV< to negatively marked termitull, must ~ considaed as Negative. 3) While tracing a closed path, select a11y 011c dircctilm clockwise or anticlockwiu. This selection is totally indq~mdent of the directions of currents and' voltages of various branches of that closed path. 1.14.4 Application of KVL to a Closed Path Consider a closed path of a complex network with various branch currents assumed as shown in the Fig. 1.46 (a). As the loop is assumed to be a part of complex network, the branch currents are assumed to be different from each other. Due to these currents the various voltage drops taken place across various resistances are marked as shown in the Fig. 1.46 (b). B
I
R1
E1
- n;l I l
~-----
+
1'2111B
Rise
e,
Rise
•
1z -
R, ~ Drop
Fig. 1.46 (a), (b) Closed loop of a complex nehNork Copyngh!cd materia
Circuit Theory
1 • 35
Basic Circuit Analysis & Network Reduction Techniques
The polarity of voltage drop along the current di.rection is to be !fllarlced a.s positive (+) to negative (- ). Let us trace this clo.sed path in clockwise direction I.e. A-B.C-0-A. Across R1 there l< voltage drop 11 R1 and as getting traced from +Ve to -ve, it is drop and must be taken as negative while a pplying KVL Battery E 1 is getting traced from negative to positive i.e. it is a rise hence must be considered as positive.
Across Rz there is a voltage drop 12 R 2 and as getting traced from ·+ve to -ve, it is drop and must be taken negative. Across R 3 there is a drop !3 R3 and as getting traced from +ve to -ve, it is drop and must be taken as negative. Across R4 there is drop I4 R4 and as getting traced from +ve to - ve, it is drop must be ta.ken as negative. Battery Ez is getting traced from - ve to +ve, it is rise and must be taken as positive. :. We can write an equation by using KVL around this closed path as, -I t R1 + Et -lz Rz -13 R 3 - !4 R4 + Ez = 0
i.e.
... Required I
Et + Ez =It Rt +lzRz +I3R3 +I4R4
If we trace the closed loop in opposite direction i.e. along A·D-C·B-A and follow the same sign convention, the re;ulting equation will be same as what we have obtained above. Key Point : So while applying KVL, direction in which loop is to be traced important but following the sign con~1tion is most important.
is not
The same sign convention is followed in this book to solve the problems.
1.14.5 Steps to Apply Kirchhoffs Laws to Get Networtc Equations The steps are stated based on the branch current method. Step 1 : Draw the circuit diagram from the given information and insert all the values of sources with appropriate polarities and all the resistances. Mark aU the branch currents with some assumed directions using KCL at various nodes and junction points. Kept the number of unknown currents minimum as far as possible to limit the mathematical calculations required to solve them later on.
Step 2 :
Assumed directions may be wrong, in such case answer of such current will be mathematically negative which indicates the correct direction of the current A particular current leaving a particular source has some magnitude, then same magnitude of current should enter that source after travelling through various branches of the network
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Circuit Theory
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Basic Circuit Analysis & Networtl Reduction Techniques
Step 3 : Mark all the polarities of voltage drops and rises as per directions of the assumed branch cu.r rents flowing through various branch resistances of the network. 1lUs is necessary for application of KVL to various closed loops. Step 4 : Apply KVL to different closed paths in the network and obtain the corresponding equations. Each equation must contain some element which is not considered i~ any previous equation. Key Point : KVL must II<' applied to sufficient number of loops such tlult tllch dement of
tire network is inclutkd atltJISI once in any of tire equations. Step 5 : Solve the simultaneous equations for the unknown currents. From these currents unknown voltages and power consumption in different resistances can be calculated. What to do if current source exists ? Key Point : If tlrert is current source in tire ndwork thtn compltlt tht currtnt distribution considering tire current source. But whik applying KVl. the loops should not II<' considered inooltring current source. The loop tqiUitions must II<' written to ~ loops whicll do not include any current source. This is because drop llCTOSS current source is unknown.
For example, consider the circuit shown in the Fig. 1.47. The C\lrrel\t clistribution is completed in of current source value. Then KVL must be applied to the loop bcdcb, which does not include current source. The loop abefa should not be used for KVL application, as it includes current source. Its effect is already considered at the time of current distribution.
/lAII!!I+.SS!il:ll'-,lilt!".,. HI ciS 1 ) 1 0 This loop 8 1 6/Jr.tllllll!::,.. ,---'>IIM--i'"'-.....:..IIJI.'Jv--lc can not be (5-1,) considered lor application ol KVL • •
SA
e
(5 - J,)
!'.: ~ ~r=
considered in of current disllibulion.
10V
d
Fig. 1.47
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Circuit ThiKifY
1 • 37
Basic Circuit Analysis & Network Reduction Technlq~,~ea
1.15 Cramer's Rule If the network is complex, the number of equations i.e. unknowns increases. In such case, the solution of simultaneous equations can be obtained by Cnmer's Rule for determinants. Let us assume that set of simultaneous equations obtained is, as follows : 8J1Xt +a12X2+ ·····••• +8tnXn :
Ct
•2t"t +aux2+ ........ +a2n xn = ~
Where C1 ,C2 , .••.. •. ••• ... •. c. are constants. Then Cramer's rule says that form a system determinant 6 or D as,
=
D
Then obtain the subdeterminants Djby replacing jtb column of 6 by the column of constants existing on right hand side of equations i.e. C1,C2 , •• • Cn;
01
~
c, •tz
"'"
•11
c,
Cz
•22
a2n
• zt 02 =
C2
c.
•n2
3nn
•t2
c,
• 21 •22
Cz
•••
Cn
•11
and
Dn
=
'n2
.., c.
•tn •zn 8nn
The unknowns of the equations arc given by Cramer's rule as,
D, x, = 1)' Where
D 1,
0 2 , ... ,
Dn
Xz
Dz = D ' ..............,
x.
On
=D
and D are values of the respective determinants,
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Cln:ult Theory
1 - 38
1-+
Apply Kirchhoffs current law and !"'llage law to lk circuit shown in the
Example 1.8 : Fig. 1.48.
..
Basic Cln:ult Analysis & Network Reduction Techniques
lndialte the various brRnch currents. Write down lk equations refilling lk various lmmch curretlls.
300
150
,.
••
•
So/VI! these equations to find IN values of these currmts.
SOV ': ="
Is the sign negati!N! ?
Flg. 1.48
If yes,
of
any of the calcu/altd currents
explain the signifiCJlTict of the negaliVI! sign.
Solution : Application of Kirchhoff's law : Step 1 and 2 : Draw the d rcuit with all the values which are same as the given network. Mark all the branch currents starting from +ve of any of the source, say +ve of 50 V source. Step 3 : Mark all the polarities for different voltages across the resistances. This is combined with step 2 shown in the network below in Fig. 1.48 (a). t, - lz 300 8 ' • • ··- lz • ··150
A
'•
• sov-::-
F
Step 4 :
•
200
E
'•
Fig. 1.48 (a) Apply KVL to different loops.
c t, - 12
•
··-·2
100V
D
Loop 1 : A-8-E-P-A.,
- 15 11 - 20
lz + 50
• 0
... (I)
lv - 100 + 20 1z = o
... (2)
Loop 2 : B-C-D-E-0, - 30 (II -
Rewriting all the equations, taking constants on one side.
15 11 + 20
lz =
50
...(1)
and
- 30 11 + 50
lz
= 100
...(3)
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Circuit Theory
1 • 39
Basic Circuit Analysis & Network Reduction Techniques
Apply uamer's rule,
Calculating 0 1,
115 201
0 = - 30 50 = 1350
o,
,, Calcula ling 0 2,
=
II: 50201
= 500
= 500 = 03 7 A = Dt 0 1350
02 = 12 =
15
so
I
- 30 100 = 1 02
D
3000
3000 = 1350 = 2.22 A
For 11 and 12, as answer is positive, assumed direction is correct. :. For I1 answer is 0.37 A. For I2 answer is 2.22 A. 11 - I2
=
0.37 - 2.22
= -1.85 A Negative sign Indicates assumed direction Is wrong.
i.e. I1 - I 2 = 1.85 A flowing i.n opposite direction to that of the assumed direction.
1.16 A.C. Fundamentals Let us discuss in brief, the fundamentals of altemabng circuits consisting of various alternating current and voltage sources, resistances alongwith inductive and capacitive
reactances. An alternating quantity is the one which changes periodically both in magnitude and direction.
Generated o.mJ.
Amplitude
Practically a purely sinusoidal waveform is accepted as a standard alternating waveform for alternating voltages and currents, d ue to its advantages. Let us consider the waveform of an alternating quantity which is purely sinusoidal as shown in the Fig. 1.49.
lime period T seconds
onecyde
Fig. 1.49 Waveform of an alternating e.m.f.
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Circuit Theoty
1 • 40
Bale Circuit Analyals & Network Reduction Techniques
1.16.1 Instantaneous Value The value of an alternating quantity at a particular instant is known as its instantaneous value. e.g. e1 and e2 are the instantaneous values of an alternating e.m.f. at the instants t 1 and ~ respectively shown in the Fig. 1.49.
1.16.2 Waveform The graph of instantaneous values of an alternating quantity plotted against time in called its waveform.
1.16.3 Cycle Each repetition of a set of positive and negative instantaneous values of the alternating quantity is called a cycle. Such repetition occurs at regular interval of time. Such a waveform which exhibits variations that reoccur after a regular time interval is called periodic waveform. A cycle can also be defined as that interval of time during which a complete set of non-repeating events or wave form variations occur (containing positive as wcll as negative loops). One such cycle of the alternating quantity is shown in the Fig. 1.49. Key Point: One cycle corresponds to 2n radians or 360°.
1.16.4 Time Period (T) The time taken by an alternating quantity to complete its one cycle is known as Its time period denoted by T seconds. After every T seconds, the cycle of an alternating quantity repeats. This is shown in the Fig. 1.49.
1.16.5 Frequency (f) The number of cycles completed by an alternating quantity per second is known as its frequency. It is denoted by f and it is measured in cycles I second which is known as Hertz, denoted as Hz. As time period T is time for one cycle i.e. seconds I cycle and frequency is cycles/second, we can say that frequency is reciprocal of the time period. V.i
v.l
..
., flme
~----H~hT----~
Less number of cycles per second I.e. low frequency
Less T
-More number of cyCles per second i.e
high frequency
Fig. 1.50 Relatio n between T and f Copyrgh!cd malcri~
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1 • 41
A~
time period increases, frequency decreases while as time period decreases, frequency increases. This Is shown in the Fig. 1.50. ; I
In our nation, standard frequency of alternating voltages and currents is 50 H7_
I
1.16.6 Amplitude The maximum value attained by an alternating quantity during positive or negative hall cycle is called its amplitude. It is denotL'
1.16.7 Angular
Frequency(~
It is the frequency expressed in electrical radians per second. As one cycle of an alternating quantity corresponds to 2 It radians, the angular frequency can be expressed as (2 n >< cycles/sec.) It is denoted by • ro' and its unit is radians/second. Now, cycles/ sec. means frequency. Hence the relation between frequency 'f' and angular frequency · ro' is,
I
2 nf
Ill =
radians/sec.
or
oo =
:.;.
radians/sec.
I
1.16.8 Equation of an Alternating Quantity As alternating quantity is sinusoidal in nature, its quation is expressed u~ing sin where 6 is angle expressed in radians. Hence alternating voltage is expressed as,
I
c= fmsinO
a
I
While alternating current is expressed as,
I
i
= lmsinO
I
This equation gives instantaneous values of an •ltem•ting quantity, •t any time t. Now
a
=
rot
in radians
Thus various forms of the equation of an alternating quantity are, e
and
t)
=
2 fmsin (rot)= Em sin (2n f I) = Em sin ( ;
=
2 lm sin (Cill) = 1, sin (2rt f I) = I, sin ( ; t)
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Important Note : In all the above equations, tl1e angle 6 is expressed in radians. Hence,
while calculating the instatJtaneous value of tht t.mf, it i.~ necessary to CtJiculatt the sine of the expressed in radians. Key Point: Made of the calculator should be converted to radillns, teo calculate tht sine of 1/u: angle expressed in radians, before substiluti11g in any of the above equations.
at~gle
In practice the alternating quantities are expressed in of their r.m.s. values. The relation between r.m.s value and the maximum value is,
I
Yr.ms
and
= V.n .J2
Ir.m.s -72, - 1,.
I
The r.m.s values are denoted by the capital letters as V or I.
1.17 Phasor Representation of an Alternating Quantity In the analysis of a.c. circuits, it is very difficult to deal with alt.c:mating quantities in of their waveforms and mathematical equations. The job of adding, subtracting, etc. of the two altematin.g quantities is tedious and time consuming: in of their mathematical equations. Hence, it is necessary to study a method which gives an easier way of representing an alternating quantity. Such a representation is called phasor representation of an alternating quantity.
The sinusoidally varying alternating quantity can be represented graphically by a straight line with an arrow in this method. The length of the line rep.resents the magnitude of the quantity and arrow indicates its direction. This is similar to a vector representation. · Such a line is called a phuor. Key Point: The phosors art assumed to be rolared in antic/ockwise direction. One complete cycle of a sine wave is represented by one complete rotation of a phasor. The anticlockwise direction of rotation is purely a conventional direction which has been universally adopted. Consider a phasor, rotating in anticlockwise direction, with uniforrn angular velocity, with its starting position 'a' as shown in the Fig. 1.51. If the projectio.n s of this phasor on y •
CUtr~t
c Antidockwlse \ rotation
9
9
Fig. 1.51 Phasor representation of an alternating quantity Co yrgh!cd malcri~
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Basic Circuit Analysts & Network Reduction Techniques
Y-axis arc plotted against the angle turned through'
e ',(or time as e =
w t), we get a sine
wavcfonn.
Consider the va.rious positions shown in the Fig. 1.51. 1. At point 'a', the Y-axis projection is zero. The ins tan taneous value of the current is aJso zero.
2. At point 'b', the Y-axis projection is [ I (ob) sin 0) ]. The length of the phasor is equal to the maximum value of an alternating quantity. So, in~tantaneous value of the cu.r rent at this position is I = Im sin 0, represented in the waveform. 3. At point 'c', the Y-axis projection ' oc' represents entire length of the phasor i.e. instantaneous value equal to the maximum value of current Im·
4. Similarly, at point d, the Y-axis projection becomes Im sin 0 which is the instantaneous value of the current at that instant. 5. At point 'e', the Y-axis p rojection is zero and instantaneous value of the current is z.ero at this instant.
6. Similarly, at points f, g, h the Y· axis p rojections give us instantaneous values of the current at the respective instants and when p lotted, give us n egative half cycle of the alternating quantity. Thus, if the length of the phasor is taken equal to the maximum value of the alternating quantity, then its rotation in sp ace at any instant is s uch that the length of its projection on the Y-axis gives the instantaneous value of the alternating quantity at th at particular instant. The angular velocity ' w ' in an anticlockwise direction of the phasor should be such that it completes one revolution in the same time as taken by the alternating quantity to complete one cycle i.e. 9 = wt, Where
w = 2 n f rad/sec
Points to :
In practice, the alternating quantities are represented by their r.m.s. ·v alues. Hence, the length of the phasor represents r.m.s. value of the alternating quantity. In such case, projection on Y-axis does not give directly the instantaneous value but as lm = ..fi 1, .• ,..1 the projection on Y-axis must be multiplied by ..fi to get an instantaneous value of that alternating quanl!ty. Phasors are always assumed to be rotated in antlcloc:k wlse direction.
Two allemating quantities of same frequencies can be represented on same phasor diagram.
If frequmcies of the two qwmlities are differmt, then sudr IJ!Ialltities camrot be represented on the same plulsor diagram.
Key Point:
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Baaic: Cin:uit Analysis & Network Reduction Techniques
1.18 Concept of Phase of an Alternating Quantity In the analysis of alternating quantities, it L• necessary to know the position of the phasor representing that alternating quantity at a particular instant. It is represented in tenns of angle e in radians or degrees, measured fr.1m certain reference. Thus, phase can be defined as, Phas~ : The phase of an alternating quantity at any instant is the angle ~ (in radians or degrees) travelled by the phasor representing that alternating quantity upto the instant of con~deration, measured from the reference.
2•
O=mt
Fig. 1.52 Concept of phase Let X-axis be the reference axis. So, phase of the alternating current shown in the Fig. 1.53 at the instant A is ¢ = 00. While the phase of the current at the instant B is the angle q> through which the phasor has travelled, measured from the reference axis i.e. X-axls.
In genera I, the phase ~ of an alternating quantity varies from ~ = 0 to 2 lt radians or ~ = 00 to 3600.
A
Current
~~~~~~~~--~~ 9=~
-- o Reference
T
2:t
4
lnstant
B
1 - - - T --=-----1 llme period
Fig. 1.53
Another way of defining the phase is in tenns of a time period T. The phase of an alternating quantity at any particula:r instant is the fraction of the time period (T) through which the quantity is advanced from the reference instant. Consider alternating quantity represented in the Fig. 1.53. As per above definition,. the phase of
quantity at instant A is {, while phase at instant B is
3 T. Generally, the phase is 4
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1 • 45
expressed in tenns of angle ¢ which varies from 0 to 2 n radians and measured with respect to positive x-ruc.is direction.
In of phase the equation of alternating quantity can be modified as,
I
Where
e = Em sln(wt±$)
I
9 = Phase of the alteiThlting quantity. Let us consider three cases; Case 1: $ =0°
When phase of an alternating quantity is zero, it is standard pure sinusoidal quantity having in.~tantaneous value zero at t = 0. This i~ shown in the Fig. 1.54 (a). Dse 2 : Positive phase ¢ When phase of an alternating quantity is positive it means that quantity has some positive inst.tntaneous value at t = 0. This is shown in the Pig. 1.54 (b). Dse 3 : Negative phase Q When phase of an a!tem.lting quantity is negative it means that quantity has some negative inst.tnt.tneous value at t = 0. This is shown in the Fig. 1.54 (c). Voltage
or
Vottage
vonage
current
or
or
current
current +Ve
t =0
~~~(@Jl}ml! Phase ~=
o•
:'
-o:
!
. / - Phasor
------~L -
t
0 Phasor
Negative phase - o
Positive phase $
diagram
''
Phasor •
diagram 't-
~
o
diagram
(ajZero phase
' _____ _o~· - ----
(bl Poaltiva phaao
(cl NogaUvo phase
Fig. 1.54 Concept of phase
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Basic Circuit Analysis & Network Reduction Techniques
1. The phase is measured with respect to reference direction i.e. positive x axis direction. 2. The phase measured in anliclockwise direction is positive while the phase measun.>d in clockwise direction is neg~tive.
1.18.1 Phase Difference Consider the two alternating quantities having same frequency f Hz having different maximum values. e
Em sin (w I) ~
and
Im sin (w t)
Em > Im
where
The phasor representation and waveforms of both the quantities a.re shown in the Fig. 1.55.
'"
!-l---:=-1--t~--.\···-······E,II 0
0 =WI
Fig. 1.55 The phasors
OA
and After 0 ~
7t
2
radians, the OA p hasor achieves its maximum E, while at the same
instant, the 08 phasor achieves its maximum ~· As the frequency of both is same, the angular velocity w of both is also the same. So, they rotate together in synchronism. So, at any instant, w e can say that the phase of voltage e will be same as phase of i. Thus, the angle traveUcd by both within a particular time is always ·t he same. So, the difference between the p hases of the two quantities is zero at any instant. The difference between the phases of the two alternating quantities is caiied the phase difference
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which is nothing but the angle difference between the two phasors representing the two alternating quantities. Kay Point : When s11ch phase diflnence bet-.uern the two altern11ting quantities is ::.eru,
the hvo quantities are said to be in p/rase. The two alternating quantities having same frequency, reaching ma ximum positive and negative values and zero values a t the same time are said to !be in phase. Their amplitudes may be different In the a .c. analysis, it is not necessary that aU the alternating quantities must be always
in phase. It is possible that if one is achicv;ng its zero value, at the same instant, the other is having some negative value or positive value. Such two quantities arc said to have phase difference between them. If there is difference between the phases (angles) of the two quantities, expressed in degrees or radians at any particular Instant, then as both rotate with same speed, this difference remains same at all the instants. Consider an e.m.f. hav;ng maximum value Em and cu.rrcnt hav;ng maximum value lm. Now, when c.m.f. 'e' is at its zero value, the current 'i' has some negative value as shown in the Fig. 1.56. e,i
... ,.....
••
/•
...
..... .f .......
. ..
. , __j__ __f.-....- : l
/.
!
\
',
\
Of
•
'.. •.,.
0
I
....
........ .
....
~
__________
' :A
'• (I) ' ~~~-i·--···
I / :
'
~•
\
\.
:
;
E,
........
-··+--::.,-_-------''1--~-.:,._
I
•
•
.. .. B·------~, ...- - - - · · - - - ·· ·· ,• -lm
/l'l ..
.
..
f)
..............,_....:.;·_·______::-1---------"-- - - -Em
Fig. 1.56 Concept of phase difference (Lag)
Thus, thef" eJrists a phase difference 9 between the two phasors. Now, as the two are rotating in anticlockwisc direction, we can say that current is falling back with respect to
voltage, at aU the times by angle \) . This is called lagging phase difference. The current i is said to lag the voltage e by angle <1> • The current i achieves its m.axi.ma, zero values 4> angle later than the corresponding maximum, zero values of voltage. The equations of th.e two quantities arc written as,
e = Em sin rot
and
i = lm sin (rot-~
'i' is said to lag 'e' by nngle $.
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Basic Circuit Analysis & Networtl R.eduction Techniques
It is possible in practico: that the current 'i' may have some positive value when voltage 'e' is zero. 1lUs is shown in the Fig. 1.57.
Fig. 1.57 Concept of phase difference (Lead)
It can be seen that there exists a phase difference of oangle between the two. But in this case, current 'i' is ahead of voltage 'e', as both are rotating in anticlockwise direction with same speed. Thus, current is said to be leading with respect to vo ltage and the pha~ difference is called luding phue difference. The current I achieves its maximum, zero values 9 angle before than the corresponding maximum. zero values of the voltage. At all instants, current i is going to remain ahead of voltage 'e' by angle 'fl. The equations of such two quantities are written as
e
~
Emsincot
and
i~Imsin(cot+~
' i' is said to lead 'e' by angle $. Key Point : Thus, rtlaJed to the plulse difftrenee, it can be remnnbered that a plus(+) sign of angle indicates lead where as a minus (-) sign of angle indicates lag with respect to the rtfertJtee.
1.18.2 Phasor Diagram The diagram in which different alternating quantities of the same frequency, sinusoidal in nature are represented by individual phasors indicating exact phase interrelationships is known as phasor diagram. The phasors are rotating in anliclockwise direction with an angular velocity of co= 2 1t f rad/sec. H ence, all phasors have a particular fixed position wi th respect to each other. Key Point : Hence, p}lflS<)r dingram can be considered as a still picture of tlrese phasors at a
particular instant. To clear this point, consider two alternating quantities in phase with each other. e
~
E,., sin co t
and
i
~ 1m
sin cot Copyrgh!ed malcri~
Circuit Theory
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Basic Circuit Analysis & Networtl Reduction Techniques
At any instant, phase difference between them is zero i.e. angle diffe rence between the two phasors is zero. Hence, the phasor diagram for such case drawn at different instants will be alike giving us the same information that two quantities are in :phase. The phasor diagram drawn a t different instants are shown in the Fig. 1.58. E~
!-- - -:, - --
0
E~
~
0
0
Fig. 1.58 Same phasor diagram at different Instants
Consider another example where current i is lagging vollage c by angle ¢. So, difference between the angles of the pha>Ors representing the two quantities is angle 9 . e = E, sin ro t
= lm sin (rot -
and
¢)
The phasor diagram for such case, at various instants will be same, as shown in the Fig . 1.59 (a), (b) and (c).
eJ
0
--
Em
\
9
1m Lagging
/
Lagging
/ 1m Lagging
9
[Em
lm
0
0
Fig. 1.59
The phasor diagram drawn at any instant gives the same information. Key Point : tluit the liigging and ltadlng W<>fll l; fl!latlvt to lilt refernru. In tlze above CJZS<, if we take current as rcfererrce, we luwe to say tltot tire voltage ICDds current by angle
• '[he directwn of rotation of pltosors is always a11ticlockwist. Important Points Regarding Phasor Diagram : 1) As phasor diagram can be drawn at any instant, X and Y rucis are not included in
it. But, gcneraUy, the refcr~'flce phasor chosen is shown along the positive X axis direction and at th.1t instant other phasors are shown. This is just from convenience point of view. Th e individu~l phase of an alternating q uantity is always referred with respect to th e positive x-axis direction. Copyrghicd malcri~
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2) There may be more than two quantities represented in phasor diagram. Some of them may be current and some may be voltages or any other illtcmating quantities like flux, etc. lbe frequency of aU of them mus t be the same. 3)
Generally, length of phasor is drawn L'CJUal to r.m.s. value of an alternating quantity, rather than max.imum value.
4) The phasors which are ahead, in anticlor.kwise direction, with. respect to reference
phasor a.r e said to be leading with respect to reference and phasors behind arc said to be lagging.
l•
5) Different arrow heads may be used to differentiate phasors drawn for different altem.tting'quantities like current, voltage, flux, etc. Example 1.9 : Two sinusoidal cu"cnts arc given by, i1 = 10 sin (rot + W3J and
i 2 = 15 sin (rot - 'lr/4)
''
'/
Calculate the phase difference between them in degrees. radians i.e.
6()0
''
n/3
Solution : The phase of current i 1 is
'
while the phase of the current
i 2 is - n/4 radians i.e. - 45°. This is shown in the Fig. 1.60.
Hence the phase difference between the two is, o = 01
-
The individual phases 60' and - 45° 0
_ ------- - - -
arewHhrespectto
•ve x-axis direction
02 = 60' - (- 45") = 105•
And i 2 lags i 1•
Fig. 1.60
1.19 Mathematical Representation of Phasor Any phasor can be represented mathematically in two ways, 1) Polar co-ordinate system Let
i =
and
I., sin (wt
2) Rectangular co-ordinate system + ¢l
The phase of current i is 9. The phase is always with respect the x-axis as shown in the Fig. 1.61.
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Basic Circuit Analysis & Network Reduction Techniques
1 ·51
I I
c ··------------
I(OA) = I, = r
A
polar syst~m, the phasor is represented as. r L ± 9. So current i above, is represented as I, L + i> in polar system. In rectangular system, the phasor is divided into x and y components i.e. real and imaginary components as x ± j y. The current i above is represented as, lm cos i> + j im sin 9 in rectangular system.
Fig. 1.61
r
phase = + 9
In
r
Polar system,
and
L
± ¢ while
= r cos
and
X
while
r = Jx2+y2,
Rectangular system, x ± j y y=rsin$ ...(1)
9= tan· I(~)
... (2)
The equations (1) and (2) can be used to convert rectangular form to polar or vice versa. Such rectangular to polar and polar to rectangular conversion is often required in phasor mathematical operations like addition, subtraction, multiplication and division. Key Point : Instead of using above rtlations, sh1dmts can use the polar to rectangular (P-+ Rl and rectangular to polar (R -+ P) functions available on calculator for lht required con~JUSions.
As the gt'aphical method is time consuming which includes plottin,g the phasors to the scale, generally, analytical method is used. Also, graphical method may give certain error which will vary from person to person depending upon the skills of plotting the phasors. The answer by analytical method is a.lways accurate. Very Important : Tire polar fonll of eqomtion or pllasc as,
1111
e = Em
altmrnting quantity ca11 be easily obtniucd frou< its sin(Cllt±~
then
E i11 polar = E L±~ whtre E = r.nu. v alue ,...
Example 1.10 : Write the polAr fonn of tire voltage given by, V = 100 sin (100 n I+ n/ 6) V
Obtain its rectangular fqnn. Solution : Vm = 100 V and¢ =
+~ rad = +30°, v,,m_<. = ~
= 70.7106 V
CoPY
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Circuit Theory
1 • 52
In polar form =
Baalc Circuit Analyala & Network Reduction Technlquea
70.7106 L + 30° V
:. Rectangular form = 61.2371 + j 35.3553 V
of an altmrating qwmtity aists in its polAr form and tlbt in rectangu/IIT form. Tlrtu to find r.m.s. valru of an alternJJting qumdity e:qnus it in polar form. , . Example 1.11 : find r.m.s. t1alut and phRse of the current l = 25 + j 4Q A. Key Point: 1k r.m.s. u/Que
Solution : The r.nu. value is not 25 or 4Q as it exists in polar form. Converting it to polar form, I = 47.1699L57.99° A "' Ir.m._ L 'A
r.m.s. value of current = 47.1699 A Phase = 57.99° Key Point: To obtain phRse, express 1M equation in sint form
if givm in cosine as,
u
e = Em cos (rut)
then
e = Em sin (rut + 90) as sin(90 + e) = cos 9
Thus the phase is 90• and not zero. In general,
e = Em e<,.;( rot± qt
then
e = Em The phase =
,.
sin(rot +90±~
90±~
Example 1.12 : A wltagt is defined as - Em cos Oll. Express it in polAr form.
Solution : To express a voltage in polar form expres.• it in the form, e = E,. sin rut Now
e = -Emroswt = -Emsin(rut+¥) 3
= Em sin ( Clll+ ; )
assin(CJlt+¥)=coswt as sin (n+ll) = - sln 0
Now it can be expressed in polar form as, 3n e = Em L + ·rad = Em L + 2.700 V
2
But + 210• phase is nothing but - 90° e = EmL-90"V
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1.20 Multiplication and Division of Phasors In th~ last section, th~ addition and subtraction of phasors is discussed, which is to be carried out using rectangular form of phasors. But the rectangular form is not suitable to perform multiplication and division of phasors. Hence multiplication and division must be performed using polar form of the phasors. Let P and Q be the two phasors such that, and
p = XJ +jyl
To obtain the multiplication Px Q both must be expressed in polar Corm P
and
q L¢1
Q = r2 L¢2
Then Key Point : Thus itl multiplication of complex 1111mbers
i11
polar fonn, the magnitudes get
multiplied while their angles get added. th~
The result then can be expressed back to rectangular form, if required. Now consider division of the phasors P and Q .
..!: Q
= fJ LQJ
r2L¢2
=I'rJ! 21 L¢1 - Qz
Key Point : Tlws in division of compltr 11umbers in polar form, the trrAgllitudts get divided
wlrile their angles get subtracted. Note : For converting polar to rectangular form, the students can use the function PH R on calculators without using basic conversion expressions. Similarly for rectangular to polar conversion, the students can use the function R H P on calculators without using basic conversion expressions. :
While <~di1ition and subtraction, use reclal•gular form. While mu1tiplication and division, usc polar form.
1.21 Impedance In the alternating circuits alonb•with the resistances, inductances and capacitances also play an important role.
The inductances are represented by inductive reactances in a.c. circults. An inductive reactance is the ohmic representation of an inductance denoted as XL and given by,
I
XL =
(I)
L=2
1t
f L !l
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Circuit Theory
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Basic Circuit Analysis & Network Reduction Techniques
The capacitances arc represented by capacitive reactances in a.c. circtrits. A capacitive reactance is the ohmic representation of a capacitance denoted as Xc and given by, 1
1
Xc = roe = 21tfC n The combination of R, XL and Xc present in the circuit is called an Impedance of the circuit. The Impedance is denoted by letter Z. But the behaviour of R, L and C is different from each other in a.c. circtrits hence R, XI. and Xc cannot be algebraically added to find total impedance of the circuit. Let us summarize the behaviour of R L and C in the tabular form. Parameter
Punt rctaistance R Pure Inductance l
Cha..cterlstlcs
v and inphase
I
•••
I logo V by 90"
Impedance In noctangular form
Impedance In polar form
Z • R+jO
Z • R <: O'
Z=O+JXL
Z = Xt_ L +90'
v rv Phasor dlag..m
I
I Pure capacitance c
I leads V by 90•
Z=O - JJ
Z=Xc <:- 90'
LV
Table 1.4 Inductive reactances are represented by positive sign + XL in the impedance while capacitive reactances are represented by neg.otive s ign - Xc in the impedance. Thus for R • L series circuit, the impedance is represented as,
z where
IZ I
= R + J x._ = =
IZI ..::o•n
J R2 +(Xd 2
and 8 = tan-1
xi
In such circuit, current lags voltage by angle 0.
For R..C series circuit, the impedance is represented as,
Z = R -J Xc =IZI.<:O" where
IZI = ~ R2 +(Xc)2
In this case 0 is negative and current leads voltage by angle 0.
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Basic Circuit Analysis & Network Reduction Techniques
Find out tilt resistance a11d inductance or CDparitaPict of tire impeda11ces if frequency is 50 Hz. i) 25 L 45" C! iii 6 + j 8 !l iiil 8 - j 10 Cl
,..,. Example 1.13 :
give~~
Solution : i) Z = 25 L 45" !l
Converting to rectangular fonn,
z = 17.68 + J 17.68 n Comparing with z = R + j Xt n n
R = 17.68 Now
Xt.
=
n
2nfl 68 =2n17·xSO =0.0562 H
:. L ii)
XL = 17.68
and
z=6 +i8n
Comparing with Z = R + j XL Q .. R = 6
n
8
Now iii)
Xt = 8 n
and
= 2n xSO = 0.0254 H
z = s - i 10 n
Comparing with. Z = R - j X c :. R =
Now
sn
and
Xc
=
1 2nfC
:. c
=
I 2nfXc
Xc = 10
I
2rtx50xl0
n
= 3.18 X 10-4 F = 318 IJ.F
1.22 Power Factor The numerical value of cosine of the phase angle between the applied voltage and the current drawn from the s~pply voltage gives the power factor.
It is also defined as the ratio of resistance to the impedance. It is denoted as cos<>·
1cos q, = p .f. = For pure L and C,
~=
~
1
90" hence the pJ. is zero.
For other combinations, the p.f. is de fined as lagging or leading i.e. whether the resultant current Jags or leads the supply voltage.
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Basic Circuit Analysis & Network Reduction Techniques
1.23 Power The power in a.c. circuit is given by, I P=V I cos¢1 where cos 0 = Power factor of the circuit. Now pure inductance and capacitance does not consume any power as cos ~ = 0 for such circuits. Only resistance consumes power. Hence power also can be obtained as, p = [ZR
where R = Resistive part of the equivalen t impedance of the circuit. Key Point: While calculating the equivalent impedance, it should be noted that while
adding tltt impedances in Sfries, the impedances must be expressed in rectangular form while multiplication and division of impedances mu..
1.24 Series R-L-C Circuit The series R·L.C circuit is shown in the Fig. 1.62. R
L
c
The impedance is given by,
z = R + i x~. - i Xc = R + j (XL - Xc)
v Fig. 1.62
If XL > Xc then resultant impedance is inductive and current I lags voltage V. If XL < Xc then resultant impedance is capacitive and current I leads voltage V. If XL = Xc then circuit becomes purely resistive
and I is in phase with V. The voltage d rops across the various clements arc denoted as V R• VL and VC' The m~gnitudes of these drops are given by, and Note that algebraic sum of VR, VL and Vc is not V as these three voltages are not in phase. But the veclor addition of VR, VL and Vc is the supply voltage V.
The network shown in the Fig. 1.63 is operatirtg in a sinusoidal steady state. Find voltage across capacitor, resistor and inductor.
,. . Example 1.14 :
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Basic Circuit Analysis & Network Reduction Techniques
sn
20mH
1 00~F
I:::::J
10 cos SOOt rv
Fig. 1.63 Solution : The applied voltage is 10 cos (500 t). Expressing it as,
v
= 10 sin (500 t + 90') . •. as sin (90 +
e) = cos e
Compare with, V = '!Im sin (
:. w = 500 rad/scc,
)i = 7.071
V
= 7.071 L 90"
v
: . V(RMS) =
:. v Now
Vm = 10 V, 0 = 90"
R = 5 0 ,L = 20mH, C = 100 IJF :. XL = roL = 10 Q
and
Xc :. Zr
=
I we= 20 n
= R + j (XL - Xc) = 5 + j (10- 20) = 5- i 10
n=
11.1803 L-63.43"0
7.071 L90" • • v :. i = - = ll.180 L - . • = 0.6324 L b3.43 A 3 63 43 ZT Hence voltages across the various elements are,
vR VL
I i I X R = 0.6324 X 5 = 3.162 v = Iil )(XL =0.6324 X 10 =6.324 v
Vc
= Iil x Xc = 0.6324 x 20 =12.648 v
=
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Circuit Theory Sr. No.
1 • 58
Basic Circuit Analysis & Network Reduction Techniqun 0
p.f . coa ~
o·
1
Unity p.f.
90'
0
Zero lagging
- 90'
0
Zero leading
D' L 9 L 90'
cos 9
Lagging
cos 0
Leading
Impedance (Zl
Circuit
Polar
Rectangular
;a n
1.
Pute R
R tt. O' Q
R•
2.
Pure L
XL L 90' !l
O+ j XL Q
3.
Pure C
Xc L -
0 -j
4.
Series RL
IZI L + 9'CI
R+ JXL f!
5.
Series RC
IZI
L - ~· n
R-jJ
90' (!
Remark
Xc!l
- 90' L
•
~
L 0
Xt > Xc Lagging 6.
Series RLC
IZI /. :t ~ n
R + j X 11 COSQ
0
X= XL - Xc
XL <
Xc Leading
Xt = Xc Unity Table 1.5 Summary of R, L and C series circuits
1.25 A.C. Parallel Circuit A parallel circuit is one in which two or more impedances are connected in parallel across the supply voltage. Each impedance may be a separate series circuit. Each impedance is called branch of the parallel circuit. The Fig. 1.64 shows a parallel circuit consisting of three impedances connected in parallel across an a.c. supply of V volts. Key Point: The voltage across all tile impedar~ces is same as supply t-ollage of V volts.
-
~------~~~------~ VvO:Is
Fig. 1.64 A.C. parallel circuit
The current taken by each impedance is different. Applying Kirchhoff's law,
... (J>hasor addition)
It + l2+l3
v
v
v
v
z.
z2
Z3
1
I
1
=
=-+~+=-
z=
~ z. · ~·~ z2 Z3
z I
Where Z is called equivalent impedance. This result is applicable for 'n' such impedances connected in parallel.
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Basic: Circuit Analysis & Network Reduction Techniquaa
1 · 59
1.25.1 Current Division for Parallel Impedances If there are two impedances connected in pa.rallcl and if IT is the total cuncnt, then current division rule can be applied to find individual branch currents.
-'• ; -IT
X ,__
-" = -IT
X ,--....:.,-
•
z2 ..::;"'= z. + Zz
:z,
Z1 + Zz
1.25.2 Concept of ittance ittance is defined as the ~iprocal of the impedance. It is denoted by Y and is measured in unit siemens or mho. Now, current equation for the circuit shown in the Fig. 1.65 is,
I
;
11 +12 + 13
I
=
V
VY
;
x(·d )+ V x(iz ) + V x(~3 )
VY1
1
+ VYz + VY3
y = Y1 + Yz +·Y3
..
where Y is the' ittance of the total circuit. The three impedances connected in parallel can be replaced by an equivalent circuit, where three ittances are connected in series, as shown in the Fig. 1.65.
~----~~}-----------J
v
L---------~~¥---------~
v
Fig. 1.65 Equivalent parallel circuit using ittances
1.25.3 Components of ittance Consider an impedance given as, Z = R±jX
Positive sign for inductive and negative for capacitive circuit. ittance
Y
= ~ =R;jX Copyrgh!cd malcri~
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Basic Circuit Analysis & Network Reduction Techniques
Rationalising the above expression, Y=
R'l'jX R'l'jX = (R ± j X)(R + j X) R2 + X2
= (R2:x2)+
i (R2:x2)=~
'!''X
I
z2
Y=G+j8
In the above expression,
G = Conductance = -
and
8 = Susceptance =
R
z2
~
z2
1.25.4 Conductance (G) It is defined as the ratio of the resistance to the square of the impedance. It is measured in the unit siemens. 1.25.5 Susceptance (B) II is defined as the ratio of the reactance to the square of the impedance. It is measured in the unit siemens.
Note :
The sign convention for the reactance and the susceptance are opposite to each
other. , Y = G + j 8 =
IY I
=
IY I
L 9 siemens or mho
,Jc 2 + B2 • o= tan-1 ~
Key Point: Impedances in parallel get 1xmoerled to illa1JCts i11 series while impedances
in series gel converted to illar1ces in parallel.
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01/cu/ate tire equivalent impedance of the 11e1tvork as vitWed tl1rnugh the temtiuats A-B showu iu the Fig. !.66. If atr altenwting voltage of 150 L {)"Vis connected across A-B, calculate tire curreut drawn from the source. Hmce carculate the pawn
,,.. Example 1.15 :
consumed. 4 + j31l
5L. Jo•n 6-jSO B
A
Fig. 1.66
Z2
6-
z3 = 5 L
Now
n = 5 L. 36.86• !l j 8 n = 10 L- 53.13• n 3o• n " 4.33 + i 2.5 n
4 + 3i
Solution : Let
z, and Z2 arc in pa.rallel, . .. : . (Z, II Zz) =
z--1Z1+Zzz--2
Z 1 Z2 must be in polar form while (2 1 :. (Z,
II Zz) "
"
Z2 ) in redangular form
5L.36.86°x lOL.-53. !3° SOL.-16.27" ( = --,.,.., ,........,.,....4+i3+6- i 8) (I 0 -j5) SOL.-16.27° 6 56• = 4.4721 L - 16.27°+26.56°
= il.lSL.-Z .
= 4.4721 L ... 10.29• " 4.4 ... ;
o.s n
4.4 + i 0.8 + 4.33 + ; 2.5 = 8.73 + i 3.3 n
= 9.332 L. + 20.706• n
This is the equivalent impedance.
150L o•
Hence the circuit becomes as shown in the Fig. 1.67 (a). V 150 L0° I = ZAO = 9 .332 L.20 .706• = 16.07 L.- 20.706• A
Figure 1.67 (a)
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Thus the current is 16.07 A, lagging voltage by angle 20.706°. The phasor diagram is shown in the Fig. 1.67 (b). The power consumed can be calculated as, P = VI cos
I
9 = 150 x 16.07 x cos( -
20706• )
= 2254.798 w
Fig. 1.67 (b)
Alternatively the power can be obtained as, p = 12 X (R.~a) Now
ZAB =
.. RAo :. p
8.73 + i 3.3 n
= 8.730
=
(16.07) 2 X 873 = 2254.4
w
This is because inductive part j 3.3 of an equivalent impedance does not consume any power.
Two impeda11ct Z1 = 5 - j 13.1 Q and Z 1 = 8.57 + j 6.42 n are connected in parallel across a voltage of (100 + j200) t'()/ts. Estimate:i) Branch cu"mts in complex form ii) Total power corrsumed, Draw a neat phasor ditlgram showing voltage, lmmcl1 cummts ~ud all phase angles.
II~ Example 1.16 :
Solutlon : The circuit is shown in the Fig. 1.68.
V = 100 + j 200 = 223.607 L 63.43° V
••
z,
z, =s- i 13.1 =14.021 ~
i)
L - 69 .t09• n
= s.s7 + i 6.42 = 10.71 L + 36.83• n
11 =
V
l;"
223. 607 L63..43• = 14.021 L69.109°
= 15.948 L 132.539° A Fig . 1.68 I _ 2-
= - 10.782 + I 11.75 A
V _ 223.607 L 63.43• 20.878 L 26. 6• A = 18.668 + j 9.3483 A - 10.71L+36.83• =
z2
ly = f 1 + f2 = - 10.782 + j 11.75 + 18.668 + j 9.3483
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Basic Circuit Analysis & Networit Reduction Techniques
= 7.886 + j 21.0983 A = 22.5239 L 69. s• A Q T = Angle between V and IT
= 69.5 - 63.43 = 6.075° leading Fig. 1.69
PT
= V IT cos h = 223.607 X 22.5239 X
COS (6.075)
= 5008.211 W
The phasor diagram is shown in the Fig. 1.69.
1.26 Star and Delta Conneetlon of Resistances In the complicated networks involving large number of resistances,, Kirchhoffs laws give us complex set of simultaneous equations. It is time consuming to solve such set of simultaneous equations involving large number of unknowns. In s uch a case application of Star-Delta or Delta-Star transformation, considerably reduces the complexity of the network and brings the network into a very simple form. This reduces the number of unknowns and hence network can be analysed very quickly for the required result. These transformations allow us to replace three star connected resistances of the network, by equivalent delta connected resistances, without affecting currents in other branches and vice-versa.
Let us see what is star connection ?
U the three resistances are connected in such a manner that one end of each is connected together to form a junction point called St.u point, the resistances are said to be connected in Star. The Fig. 1.70 (a) and (b) show s tar connec_!!!d-resistances. The star point is indicated a.~ S. Both the connections Fig. 1.70 (a) and (b) are exactly identical. The Flig. 1.70 (b) can be
redrawn as Fig. 1.70 (a) or vice-versa, in the circuit from simplification point of view.
s (a)
(b)
s (c)
Fig. 1.70 Star connection of thrwe resistances
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1 • 64 Basic Circuit Analyals & Network Reductio n Techniques ~-----------------------------------------------
Let ua see what Ia
d"a" connection
?
If the three resistances are connected in such a manner that one end of the first is connected to first end of second, the second end of second to fi~t end of third and so on to complete a loop then the resistances are said to be connected in Delta.
Key Point: Delta connection alW
00
00
00
Fig. 1.71 Delta connection of three resistances
1.26.1 Delta..Star Transformation Consider the three resistances Rt2 . R23 . R31 connect
1
terminals between w!tich these are connected in Delta arc named as 1. 2 and 3.
R,
s
Now it is always possible to replace these Delta COMectcd resistances by three equivalent Given Delta Fig. 1.72 connected resistances Equivalent Star Star Rt. Rz, R3 between the same terminals 1, 2. and 3. Such a Star is shown inside the Delta in the Fig. 1.72 which is called ~qulval~nt Star of Delta connected resistances. Key Point : Now to call tkse two arrangtma•ts as equivalent, the resistance belwttn any twa tenniuals must be S
2
Let us analyse Delta connection first, shown in the Fig. 1.72 (a).
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Circuit Theory
1 • 65
Basic Circuit Analysis & Networlo: Reduction Techniques ParaHel
.-------o1
~
1
2
.__ _R23 ..;__ _ _ _ _ 3
2 o---.......L----'
(a) Given Delta
Fig. 1.72
(b) Equivalent between 1 and 2
Now consjder the terminals (1) and (2). Let us find equivalent resistance between (1) and (2). We can red.raw the network as viewed from the terminals (1) and (2), without considering terminal (3). This is shown in the Fig. 1.72(b). Now terminal '3' we are not considering, so between terminals (1) and (2) we get the combination as, R12 parallel with (R31 +R23) a.~ R31 and R23 are in series.
:. Between (1) and (2) the resistance is, =
R 1z (R31 +Rz.l) R12 +(R31 +R23)
[using : •
~2
I+
.. . (a)
for parallel combination)
Now consider the same two terminals of equivalent Star connection shown in the Fig. 1.73.
R, R,
S·
s 2 , __ __ ___,
3
Fig. 1.73 Star connection
2
Flg. 1.74 Equivalent between 1 and 2
Now as viewed from tennina.Is (1) a.n d (2) we can see that terminal (3) is not getting connected anywhere and hence is not p laying any role in deciding the resi~tance as viewed from terminals (1) and (2). And hence we can red.r aw the network as viewed through the tcrm.ina.Is (I) and (2) as shown in the Fig. 1.74. :. Between (!)and (2) the resistance is= Rt + R2
... (b)
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Cln:ult Theory
1 • 68
Basic: Cln:ult Analysis & Networ1c Reduction Tec:hnlqUM
Rz
R2., = Rtz R12 + R23 +R31
... (h)
R3
R31 = R12 R23 +R23 +R31
...(i)
Now multiply (g) and (h), (h) and (i), {I) and (g) to get foUowlng three equations. Rtz
2
R31 R23
(Rtz +R23 +RJt)
···0>
2
2 R23 Rt2 R31 (Rtz +R23 +RJt)
...(k)
2
2 R 31 R tz R23 (Rtz +R23 +RJt)
••.(!)
2
Now add O> ,{k) and (I)
=
R12 2 R3tR23 +R23 2 RtzR31 +RJt 2 Rtz R23 2 (Rtz +R23 +RJt)
=
RtzRJtR23(Ru +R2.1 +RJt) 2 (R12 +R23 +R3J) R u R 31 R23 Rtz + R23 +R31
But
Prom equation (g)
Substituting in above in RH.S. we get, RtRz +RzR3 +R3R1
I
=
Rt R23
R23 = Rz +R 3 +
R~~ 3
Similarly substituting in RH.S., remaining values, we can write relations for remaining two resistances.
and
R12
= Rt +Rz + R~:l
R31
= RJ+Rt +Rk~3
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Basic Circuit Analysis & Networtc Reduction Techniques
Equivalent dena of given star
3
Fig.
1.n
Star and equivalent Delta
Easy way of ing the result :
Tltt tquivalf.llt delta !;{JIIIti!Cttd ~TI'Sislana to be Ct>mm:teil belwi'en any two ttmti11als is >11m of the fu,'Q rcsisf4ttci'S comlt'Cied belttle!'n the same tuJO ttnnlna/s. an4 star point respectively iu stqr, plus lire product of tlte samt two star resistances divided bY tire third star rt'liMmru. So if we want equivalent delta resistance between terminals (3) and (1), then take sum of the two resistances coru\ected between same two terminals (3) and (1) and star point respectively i.e. terminal (3) to star point R 3 and terminal (1) to .star point i.e. R1 • Then to this sum of Rt and R3, add the term which is the product of the same two resistances i.e. R 1 and R 3 divided by the third star resistance which is R2 . .
RtRJ
.. We can wr1te, R31 = Rt + R 3 +~ which is same as derived .above. Result for equal resistances In star and delta : U all resistances in a Delta connection have same magnitude say R, then its equivalent Star will contain,
i.e. equivalent Star contains three equal resistances, each of magnitude one third the magnitude of the resistances connected In Delta. U all three resistances in a Star connection are of same magnitude say R, then its
equivalent Delta contains all resistances of same magnitude of , Rx R R12 = R31 = R23 = R+R +-y = 3 R
i.e. equivalent de.lta contains three resistances each of magnitude thrice the magnitude of resistances connected in Star.
Circuit Theory
1 • 70
Basic Circuit Analysis & Network Reduction Techniques
Delta.Star
Star-Delta
Equ.va!ent delta
EQUiviMent star
Table 1.6 Star-Delta and Delta-Star Transformations ,. . Example 1.17 :
Convert the given Dtlta in the Fig. 1.78 into equivalent Star.
3
150
Fig. 1.78 Solution : Its equivalent star is as shown in the Fig. 1.79. Where R1 =
10x5 1.67 0 5 + 10+15 =
R2 =
15x 10 5+10+15
= 50
=
5x15 5+10+15
= 2.5 0
R3
R,
s 3
2
Fig . 1.79
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,,... Example 1.18 : Cm1vertthe given star into an equivala1t delta. 1
3
2
Fig. 1.80 Solution : For star to delta conversion,
(4+ .3)(3 -j4)
= 4 + j 3 + 3 - j4 + ~..,'~:,.,...:....:.. (5+j0)
. 5L36.86 °X5L - 53.13 o
= 7 - J+
SLO O
= 7- j + 4.8 -; 1.4 Similarly
~
= 7 -j+SL- 16.27 °
= 11.s - j 2.4 n
and 2 31 can be obtained. The equivalent delta is shown in the Fig. 1.81.
Fig. 1.81 Key Point : Use rectangular system for addition or subtraction while polar for
multiplication or division.
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Beale Cln:ult Analyala & Networtt Reduction Technlquea
Examples with Solutions ,_. Example 1.19 : Find
resi.tllna between points A-8.
~iuaktu
60
40
Fig. 1.e2 Solution : Redraw the circuit, A o---------r------,
i'~i'='-
150
150 <
100 •
c
0 40 ~
60
""' 60 '
<
,
."~'
,, ..
4Q
~..
B
B
Fig. 1.83 (a) A
A 15 x10 15 •10
=60
"'
"' 6x4 6+4
B
a
150
=
RA·B s 6+2.4 8.40
2.40
B
Fig. 1.83 (b)
..
·. RAB = 8.40
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Basic Cin:ult Analysis & Network Reduction Techniques
n. . Example 1.20 : 01/culate the tfftdivt resisllmce betwem points A and 8 in the gi~~m circuit in Fig. 1.84. 40
30
2 A
Sll
20
60
Sll
20
20
50 B
3Cl
Fig. 1.84 Solution : The resistances 2, 2 and 3 are in series while the resistances ·4, 2, and 5 are in
series. 2+2+3 = 70 and
4+2+5 = 110
The circuit becomes as shown In Fig. 1.85 (a).
6
5 ............~................~--oB
~
Fig. 1.85 (a) Converting 6 PQR to equivalent star~
6x 3 RPN = 6+3+6 = 1.20 6x6 RPN = 6 + 3 +6 = 2.40 6x3
~N ~ 6 +3+ 6 = 1.2 o
Hence the circuit becomes as shown in the Fig. 1.85 (b).
R 5
~------~--------~~8
Fig. 1.85 (b)
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Circuit Theory
Basic Circuit Analysis & Network Reduction Techniques 3.2
The resistances 2 and 1.2 are in series.
A~.---~~---r--------~
1.2 and 11 are in series.
5 and 2.4 are in series.
7
:. Circuit becomes after simplification as shown in the Fig. 1.85 (c).
7.4 L--------L--------~~ 8
The resistances 7.4 and 12.2 are in parallel. 7.4x 122 .. 7.4 11 12.2 4.6061 n . + 7 4 122
=
Fig. 1.85 (c)
=
So circuit becomes,
3.2 A
A
7
Series
"U.
-
4.6061
B
(d)
B
(e)
Fig. 1.85
Now the two resistances arc in parallel. 7 x 7.8061 RAB = 7 +7.8061 = 3.69
Q
,._ Example 1.21 : Find the currmt in the branch A · B in the d.<:. circuit shown in the Fig. 1.86, using Kirchlroffs laws. 16A A
Hl
SA
4A
Hl B 7A
Fig. 1.86
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Circuit Theory
1 • 75
Basic Circuit Analysis & Networl\ Reduction Techniques
Solution : The various branch currents are shown in the Fig. 1.86 (a). Applying KVL to loop ADBA App¥ng KCL al various nodes
16A A
... (I) Applying KVL to the loop ACBA,
,
- (16 - 11 - l:z) - (12 - It -l:z) + It = 0
16 - ·,-~
0
c
SA
:.- 16 + 11 +
4
:.311 + 212
lz- 12 + 11 +
= 28
12 + 11 = 0 ... (2)
Add (1) and (2), B
411 = 23
7A
11 = 5.75 A
Fig. 1.86 (a)
... This is the current through branch
AB. ,_,. Example 1.22 : Determine the equiwlent resistance the circuit si10W11 in Fig. 1.87.
0
A
~tween
G
1 Cl
C
50
D
80
B
A
40
E
70
F
100
F
the terminals A and B for
B
"CEEi". Fig. 1.87
Solution : In Fig. 1.87, the resistances 2 0 and 1 0 are in series and resistances 10 0 and 9 0 are in series.
Fig. 1.87 (a)
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Circuit Theoty
Bulc: Circuit Allalysl8 & Networtl Reduction TIChniqua
1 • 76
Converting delta AEC to star
c
c
~ 30
s
<
• 40
E
Fig. 1.87 (b) 3
X
3
"' 3 + 4 + 3 "' 0·9 (} 4x3
"' 3 + 4 + 3 = 1•2 (}
3X4
Res "' 3 + 4 + 3 = 1.2
..
a
Converting Delta DB.F to star 80
0
0
B
::::::
B
s RFs
F
F
Fig. 1.87 (c) 6x8 8 + 19
..
Ros = 6 +
..
19 = 4.6()6 (} Rss = 6 +8 X8 + 19 . . .
.. ..
RPS =
= 1.4S4S (}
6 X 19 6 + 8 + 19"' 3·4545 (}
RAB "' 1.2 + (7.3545
c
50
11 11.6545)
+ 4.606 B
0
B
3.45450
A
A
E
70
f
Fig. 1.87 (d) Copyrgh!cd malcri~
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1 -77
Circuit Theory
= 12. + 7.3545 X I 1.6545 606 =10.31S O 7.3545 + I 1.6545 + 4.
4.6060 11.65450
Fig. 1.87 (e)
1-+
For the circuit shown in the Fig. 1.88, ruritt KCL al!d KVL equalion and so!N to find cumnts I1 and 12. Example 1.23 :
2Cl
Fig. 1.88
as s hown in the
Solution : Consider the various branch currents and node voltages Fig. 1..88 (a).
20
Applying KCL at node A,
A V
0
tI,
'•
12
5 1, 13
t
41,
5 11 - f3 + 12 = 0
tl2
10
13 =
Now
v; and
20
20 -Va 1
20V
Note the direction of 12 which is coming towards the node hence the 20 V source is at
B
Fig. 1.88 (a)
v.
higher potential than V• forcing 12 towards node A from the base.
20-V. = 0 1 511 = 1.5 11 = 0.3 Applying KVL to the loop ABCOA, - 2 13 + 12 - 211 = 0 511 - - + 2
v. -20 v. - 4
. .. (1)
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Basic Circuit Analysis & Network Reduction Techniques
1 • 78
-2xv•+12-2I 1 2
..
V• + 2 !1
~
0
~
12
... (2)
Pu tting 11 from (I) in to (2),
v. + 0.6 v. - 8 12 1.6 v, = 20 v. = 12.5 v ~
.. .. ..
II
and ••
=-
12 =
0.25 A i.e. 0.25 A
20-V, = 7.5 A 1
.J.
r
Using successive source tran.<Jommtion, find the voltage across 1 Cl resistor behveen 'a" and 'b" shown in the Fig. 1.89.
Example 1.24 :
10
20
Hl L---~---------------4b
Fig . 1.89 Solution : Converting all the voltage sources to the current sources, 1fl
10
2Cl
211
10
L----L----~----L------------4 b
Fig . 1.89 (a)
2111 •0.6670
211 1 = 0.667 0
Hl
L---~--------------~ b
Fig . 1.89 (b) Copynghtcd materia
Circuit Theory
1 - 79
Basic Circuit Analysis & Network Reduction Techniques 4V
0.667Q
0.66Hl
10
~------------------~b Fig. 1.89 (c) 1.3340
,----.------<jla
'•b 1.3340
Hl L----Ob
Hl
L---.l.------Ob
Fig. 1.89 (d) & (e)
l,.b
2xt.334
v•b ,. . Example 1.25:
... Current division rule.
= (1. 334+1) = 1.143 A
= I,b X 1 n = 1.143
v
with 'a' positive.
Using source transformation, find V 1 and V2 s1wum in the circuit.
2Q
2A
t
t
2(l
1A
Fig. 1.90
Solution :
Cunv~rting
all voltage sources to current sources, )Q
v, 2A
t
2
t
0.5A
2
t
1A
2
1A
Fig. 1.90 (a) Copyrghlcd malcri~
Circuit Theory
1 • 80
2.5A
Basic Circuit Analysis & Netwolil Reduction Technlqun
2112 =1 0
t
t
20
2A
Fig. 1.90 (b) 10
Converting sources,
current
sources
to
voltage
+
10
+
20
Applying KYL, - 21 - 1 - 1 - 2.5 + 4~0
+ 4V
00
-
4I = - 1.5
I = 0.375 A Drop across 2 n = 2 x 0.375 = 0.75 y
Fig. 1.90 (c) and Drop across Hl = 1 x 0.375 = 0.375 y
v,
= 0.375 + 2.5 = 2.875 V +ve with respect to base.
and
v2
= -0.75 + 4 = 3.25 V +ve with respect to bue.
,.
Example 1.26 : For tire circuit shown in tM Fig. 1.91, use source tran!;formations to detmnine currmt I. Hl
20 10 40 10
Fig. 1.91 Solution : Redrawing the given network we get,
Copyrgh!cd malcri~
Circuit Theol)'
1 • 81
Basic Circuit Analysis & Network Reduction Techniques 21l
Hl
40
20
40
Fig. 1.91 (a)
10
20
Hl
j
10--:1
1A
100
1114 =0.80
(b)
(c)
10 1.80
0.80 100
2V +
-+
100
1 •0.8 =0.8V
(d)
(e)
I
2V •
0.811.8 =0.444A
2V +
1.52540
j 0.444A
(g)
(f) 1.52540 2V
• -
+
0.444. 1.5254 =0.678 v
(h) Fig. 1.91
Copyrigh!ed malcria
Circuit Theory
1 • 82
Basic Circuit Analysis & Networtl Reduction Techniques
Applying KVL, -1.5254 X I - 0.678 ... 2 = 0
2-0.678
l.S = 0.8667 A 254
,,_. Example 1,27 : A Wheatstone bridge consists of the folluwing resistanas. Branclles AB = 3 0, BC = 6 Q, CD = 12 Q and DA = 10 n.
A 2 V cell is connected btlwten points 8 and D and ga/VQI!omder of resistance 20 Q is connected betwa:n A and C. Find the cu"ent through glllvanomder by Kircluaoffs laws. So lution : Step 1 : Circuit diagram from given inJormation. Step 2 and 3 : Mark all the branch currents applying KCL at various codes and then mark the polarities of various voltages due to these assumed branch cu.r rcnts. Step 4 : Apply KVL to various loops. 0
Loop 1 : Loop A-D-B-1\ (through cell) - 10 (!1 - 12 + IJ) + 2 - 3 (11 - lz) = 0 .. - 13 II - 13 l2 - 10 l3 = - 2
... (I)
Loop 2 : Loop A·D·C·A
.-
- 10 (!, - 12 + 13) + 12 (12 - !3) - 20 13= 0 - 10 I I- 22 '2 - 42 !3 = 0
c
2V
.. . (2)
Fig. 1.gz
A
+
-
2V
Fig. 1.92 (a) Copyrgh!cd malcri~
Circuit Theory
1 • 83
Basic Circuit Analysis & Network Reduction Techniques
Loop 3 : Loop A-8-C-A
+ 3 (11 - 12 ) - 6 ~ - 20 I3 ~ 0 ... (3)
We want current through galvanometer i.e. ~- Applying Cramer's rul!c 0 =
-13 - 10
13 - 10 22 -42
3 -9
..
-20
0 = 6156,
13 -2 - 10 22 0 3 -9 0
-13 03
;
0 3 = -48
13
~
03
D
- 48
~ 6156 = - 0.00779 A
..
Cu rrent through galvanometer is 7.79 mA but negative sign indicates its d i.reclion is from A to C.
n•• Example 1.28 : Two batttries A and 8 luzving e.m.fs of 209 V and 211 V having intenull resistance 0.3 n a11d 0.8 n respectively are to be cluzrged from a d.c. source of 225 V. If for th.lt purpose they wert connected in parallel and resistance of 4 n was connected betwem the supply and batteries to limit charging curmrt, find i) MP.grritude and direction of current through each battery. ii) Power delivered lly source. Solution : The circuit diagram is as shown in Fig. 1.93.
I,
A
We can use branch current method. Show the branch currents and polarities.
40
•
Apply KVL to different loops.
11 - 12 +
o.sn
209V
'•
... (1)
Loop 2 : Loop A·B-C·O·E-F-A, i.e. - 0.8 (I1 - Ill - 211 + 225 - 4 11 • - 4.8 11 - 0.8
12 +
Source
- 0.3 12 - 209 + 225 - 4 II = 0
i.e.
c
0.30
Loop 1 : Loop A·B-E·F·A
i.e. 4 I 1 + 0.3 I2 • 16
t, -12
B
Iz + 14
E
211
v
D
Fig. 1.93
0
• 0
... (2)
Copyrghtcd matcri~
Circuit Theory
1-U
i.e.
Basic Circuit Analysis & Networtc Reduction Tec:hnlques · 4.8 It - 0.8 12 = 14
Solving equations (1) and (2) simultaneously, It = 3.663 A 12 = 4 .482 A
It - 12 = - 0.8183 A i.e. it is in opposite direction to what is assured. i) Magnitude of current through source
= 3.663 A l
Magnitude of current through battery A = U82 A
J.
Magnitude of current through battery B = o.8183 A l ii) Power delivered by,
Source = 225 x 3.663 = 82.4.175 watts ,_. Example 1.29 :
Find tire tquilllllent resislllnct betwten 8 Rrrd C.
(.ApriVMay - 2004)
80
Fig. 1.94 Solution : Converting internal star to delta, RAB
= 3.84 + 2.4 +
Roc = 3.84 + 1.6 + RCA = 2.4 + 1.6 +
3
·~~ 2.4 = 12
3
·~~ 1.6 = s o
2.~:'s!· 6 = 5
0
Q
The circuit reduces as shown in the Fig. 1.94.
Copyngh!cd malcria
Circuit Theory
1 • 85
Basic Circuit Analysis & Network Reduction Techniques A
RAB 1211
80 B '----'WVIr----> C 8118
• 40 Shaded : Parallel combinations
(a)
{b)
Fig. 1.94 Rearranging to calculate Roc, :. Roc= (4) 11 (6 + 2.5) 4x85 = 4+8.5 = 2.72 n
Fig. 1.95
1m+
Example 1.30 :
Determine the value of R irr tire circuit tuloc• the Cllrretlt is uro in the
branch CD.
(Aprii/May-2004)
R
..
A
sn ~
? 20!l ~
~
v -:.;:-
c
A
10!:! ~
\ A.
0
::-$ R
B
Fig. 1.96 Solution : Use Kirchhoff's laws. The various branch currents are shown in the Fig. 1.96(a).
Copynghted rna .ria
Circuit Theory R
I, E
Basic Circuit Analysis & Network Reduction Techniques
1 • 86 _A
A
Current through branch CD is uro.
"
+ •
·· -
12 +
5C!_ : v ~=-
Apply KVL to EACBFE,
+
;
<
.
-
1=0
c 12
•
~
~ _<
~
F
Apply KVL to EADBFE,
+
10Cl :
- ltR-2013 -R13 + V = 0
R
:.l tR+(20+R) !3 = V
B
i.e.lt - 12 -! 3
=
... (2)
... KCL at node A.
Fig. 1.96 (a)
D
... (1)
:. Rit+l512 =V
•••
R 15 R 0 1 - I
0 20+R - 1
=0
... (3)
= 15 (20 + R) + 15 R + R (20 -+ R)
= R2 + 60R +300 R 02
03
v v
0 20+R -1
=
R 1 0
=
V (20 + R)
=
=- RV + V (20 + R) + RV
R 15
v
R 0 1 -1
v =15 V- RV + RV 0
= 15 v V (20+ R)
02 o= R2 +50R+300
..
!2
=
and
13
= PJ D
=
lSV R 2 +50R+300
To have current through CD uro, the points C and D are equipotential i.e. drop across 5 n d uc to I 2 must be same as drop across 20 n due to I 3 . .. 5 12 = 2013
.. .. ..
5x
V (20+ R) 20x15 V = 2 R2 +50R+300 R +50R+ 300 100 + 5 R = 300
R = 40 0
Copyrgh!cd malcri~
Circuit Theory
1 ••
1 • 87
Example 1.31 :
Basic Circuit Analysis & Network Reduction Techniques
Using squra lransfomtlltion, find tilL power deliutnd by !he 50 V
voltage SOilrctl.
(ApriVMay 2004)
511
30
20 50V
10V
Fig. 1.97
Solution : Converting 10 V voltage source to c:urent source and drawing a network, 10
A
I'= J = 3.333 A
50
Adding two current sources, we get single current sow-ce of value (10 + 3.333) A i.e. 13.333 A.
3.333A 10A
20 r
.
30
Find equivalent resisbl.nce for parallel connection of 2 n and 3 n i.e.
Fig. 1.97 (a)
R' = 2 X 3 = -6 = 1.2 n and redrawing a network as shown in the Fig. 1.97 (b), (2 +3) 5 A
50
I"
13.333A
1.20
Flg. 1.97 (b) Now, converting current source back to voltage source,
V' = f.
R = (13.333) (1.2) = 15.996 volts A
50
•
•
1.20
50V
Fig. 1.97 (c) Copynghlcd materia
Circuit Theory
1 - 88
Basic Circuit Analysis & Network Reduction Technlqun
Applying KVL, - 1.2 I - 15.996 + 50 - 5 I
;
0 0
..
0
I (1.2 + 5) = (50 - 15.996)·
..
I =
(50 - 15.996) (5+1. 2)
= 5.484 A
: . Power supplied by 50 V source,
p = (50) (5.484) = 274.2 watts CalculJlt~ tlu CWTtnt through 6 n usisiJlna appliallion of KircJrlwffs laws.
,_ . Example 1.32 :
~
20
givm nttumk by
[April/May-2004)
40
Hl
10V ., :;.
of the
0.
40
-:::- 20V
60
Fig. 1.98
Solution : Mark all the branch currents starting from positive of 10 V source. Mark all the polarities for different voltages across the resistances.
...
20
A
I,
B u,-12) •
+ ••
12
1
10V
+
~=H
10
40
c
"
+
13 +
40 : ~· ~
0:
60 ;
G
-
-
D
-:,; 20V -;; _
F
Fig. 1.98 (a) Now applying I
Loop 1 : A·B-G-H·A Loop 2 : 8-C-F..C.B
- 2 ·~- 4 12 + 10 = 0
... (1)
- 1 ( II - 12) - 6 ll + 4 12 = 0
. .. (2)
Copyrgh!cd malcri~
Circuit Theory
1 • 89
Basic Circuit Analysis & Network Reduction Techniques
... (3)
Loop 3 : C-0-E-F-G Rewriting above equations by taking constants on one side, 2 11+ 4 12 = 10 - 11+ 5 12 - 6 13
=0
- 4 11 + 4 12 + 10 13 = 20 D
Applying Cramer's Rule,
=
2 4 0 - 1 5 -6 =284 -4 4 10
Now we are interested in finding current through 6 n i.e. 13.
03 =
13 =
2 4 10 - 1 5 0 =440 -t 4 20 03
0 =
440 284 = 1.5492 A
As the answer is positive, assumed direction of 13 is correct. So current through 6 resistance is 1.5492 A flowing from C to F.
n
,_. Example 1.33 : Calcuh!te the resista11ce Ru when all the resistana values art equal to <April/May-2005) 1 n for the circuit in Fig. 1.99.
b
d
Fig. 1.99 Solution : Converting deltas aeb and ced to equivalent star,
1
Fig. 1.99(a) Copyrgh!cd malcri~
Circuit Theory
R
1 -90
R "~ 2 = •"3
I=
~
Basic Circuit Analysis & Network Reduction Techniques
1x1 1 1 +1 +1 - 3
n ,
The circuit reduces as shown in the Fig. 1.99 (b) Series
77
a
a
Req
e
H
•
113
113
113
~
(b)
Series
c
1/3
113
ROQ
1 +(1/3)= 4130
!•
•
1/3 + 113
2130
•
1/3 ~
b , . 113 = 4130
d
(c)
Fig. 1.99
Converting sbds delta into star, we get
• •
213
,.
• s,d
1/3 ;.
b
4/3
d
b
Fig. 1.99 (d)
Copyrgh!cd malcri~
Clrc:ult Theory
1 • 91
Basic Circ:ult Analysis & Network Reduction Techniques
The circuit reduces as shown in the Fig. 1.99 (c) a
113
-
Req
413
e
'j s' 0.38090
Patallel
~
s,d
0.19040 b (f)
Fig. 1.99
I..
~q = (!. 7!42J0.4285)+0.1904: 0.533211
Example 1.34 : An impedance consumes a PQU1" of 60 walls ami lllkes a cu"enl 10- j 8 A when conru:cted to a source of 'a + j 5' V. Find 'a' and cirCIUI tlemenls.
of
Solution : The given circuit is shown in the Fig. 1.100.
V
2 = T R + jx =
10-f8 A
a+j5 = t0-j8
t.
a +j5 10-j8
atjSV
!
Rationallsing right hand side,
Fig. 1.100
(a +j5)(10+j8) R + jx = (10-j8)(10 +j8)
=
R + jx =
(a +j5)(10+j8)
(100) -(j2 64)
lOa -40 164
= .:..(1-0a '-_ -_ 4_0;..,)+,..;i.:.;.<SO.c....+S.:..a~) 164
. 50 +8a
+1
164
... (1)
Equating real and imaginary parts,
and
R =
l Oa-40 164
... (2)
X=
50+8a 164
.. . (3)
The power consumed by impedance Z is,
Copyrigh!ed malclia
Circuit Theory
· 1 • 92 p
..
.. ..
Basic; Cln:ult Analysis & Network Reduction Tec:hnlqun
=
60
= 164 R = 0.3660
R
2
(J10 2 +8 2 )
60
xR
•.• (4)
Substituting in (2), 0.366
.. ..
=
lOa -40 164
= 40 + 0.366 X 164 a = 10 50+80 Substituting in (3), X = = o.7926 n 164
I..
10 a
•.. (5)
Hence the voltage applied is 10 +j 5 volts while the impedance is (0.366 + j0.7926) n.
Example 1.35 :
The network s!wrun in II~ Fig. 1.101 crmsists tJj two star connected
circuits in parallel. Obtain tht single tklla connected equivalent. 10
10
""""" j10
""""" 'j",'Q
5
~ap
•
I
Fig . 1.1 01
Solution : Converting both the stars to delta, .
.
Zt = JIO + JIO +
''
'
$>,, ,,<1: 5 ''
' ,,
,,
,
j!Ox jlO
5
.
= - 20 + ]20
~
= jlO + 5 +
jl~~ 5 = 10 + jlO
Z:l
= jlO + 5 +
jl~~ 5 = 10 + jlO
z; = 10 + 10 +
10
~10 = 20 -
;2o
... .,.1 =- J. I
Fig. 1.101 (a)
Copyrghtcd malcri~
Cln:ult Theory
Basic Circuit Analysis & Network Reduction Techniqun
1 • 93
z',
,
~---------c::t --------: :
10
''
'
10
~' '
:
,, ' ' ,,
,,
,
.
z 2 = 10 + 1s +
lOx jS . -w = to + 11o
, . lOx jS z 3 = 10 + 1s +
--ro- ~ 10 + 1.1o
Connecting both the deltas we get the circuit as shown in the Fig. 1.101 (c).
Fig. 1.101 (b)
z
z,
z• = (- 20+ J20) (20 - j20) 1
-
20+ j20 + 20- j20
= .. open circuit
z, Zi
l 11
Z:! II Z2 = (10 + j10) II (10 + j10)
Z:J
= S + jS ~ II Z'3 = S+jS
Fig. 1.101 (c) So effective single delta connected circuit is as shown in the Fig. 1.101 (d).
Fig 1.101 (d)
,,... Example 1.36 :
Obt4in lht thiiA connected equivalent of tht ndwork show11 in Fig.1.102. -J2n
---1:
i~!l-
-~
Fig. 1.102
Copyrgh!cd malcri~
Circuit Theory
1 • 94
Basic Clreult Analysis & Network Reduction Techniques
Solution ; Consider a star network formed with - j2 Fig. 1.102 (a).
n,
j5
n
and 5
n
as shown in
Ze
,·-- -t=J- --, ' -j2Cl
·• : I'
o '
z..
Parallel
jSQ
"""""
II
; 50
•
'
OZc .
-7.5+j5)Q
100
(a)
10Cl
(b)
Fig. 1.102 Converting star network into its equivalent d elta network as follows. zA = - j2 + 5 +
H~~ <5 rel="nofollow"> = - 12 +5-2 = (3- j2) n
z 8 = - j2 + j5 +
<-i 2~ (jS) =- 12 + J5- 2 = (2- j3) n
Zc
= j5 + 5 +
12.5
= (- 7.s
+ j5) n
Replacing sta.r network by its equivalent delta network as shown in the Fig.1.102(b). It is dear that Zc and 10 n in parallel. H ence we can write, Z(: = Zc ll l 0={- 7.5+j5)(10) = (- 7.5 +j5)(10) - 7.5+j5 + 10 2.5 + j5
= (9 . 0138 Ll46 . 3" )(10 L O") : 16 .1245 L S:!.ll7' (5 .5901 L63 .43" ) = (2+j16)Q Hence delta connected equivnlent of the ootwork is as shown in the Fig. 1.102 (c).
(2+]3)0
(3-]2)0
z,.
Zc
(2+j16)fl
Fig. 1.102 (c)
Copyrghlcd matcM~
Cln:ult Theory
1 • 98 Basic Cln:uit Analysis & Network Reduction Techniques ----------------------~------------------------
!1. Find tht equill
iii A and N
lAns. : u1.33 n
m0.11n 1
A
8
6U
Flg. 1.107 12. Detmnint ammt In bran
150
200
150
A
300
300
B
Fig. 1.108 13. In tht following circuit, dtlmnine I) It, h and 1), iiJ Valou of R and
iii) Volou of Ex
(Ant.: l1 • 0.3 A. h •1.5 A. E, • 174 V,l3 • 0.7 A, R •11.4!l) A
Fig. 1.109
Copyrghlcd malcri~
Circuit Theory
1 • 99
Basic Circuit Analysis & Network Reduction Techniques
14. Rtdu« lilt mtwork,using souru trrmsfomulfiQn IU105S tM
A-B.
lnmi71Als
A
211 ~ 10V
+ 3A
211
2ll
~
8
Fig. 1.110 15. Deriw tM rel41iol15hip to express thm stor tonnttUd resistJin«> into "'"iOJiimt deltJI.
16. Deriw the reWiDmlrip to express three th/14 .,._ted r<>istiUices into equiOJiimt slllr. 17. Two vo/lmeltrs A and 8, having rtsisllmt:ts of 5.2 1<0 and 15 1<0 resp«tiody are "'"ntdtd in serils IUTOSS 240 V supply. Wh.ot is lilt reAding on =h voltmeter ? (Ana. : 61.78 V, 118.21 V) and 20 n art conntdtd in pamllel. A r<Sistana of 12 n is =ntdtd in serils wifh the combi7Ultiott . A voltagt of 120 V is 11pplitd IUTOSS the entirt tirtuit. Find lilt
18. Two resisllm«> 15
n
turrtnl in tatlt resistance. vollngt across 12 n T<Sisliln« and pow
two resistunces of 12 and 8 n. Tht total pow
19. A mistance R is ~ in suits with a parlllkl circuit comprising
20. In the series parallt l circuit shown in lilt Fig. 1.111.find the ii) lilt supply voltage V i) voltage drop tM 4 0 resistanct
=
(Ani.: 45 v, 140 V) A
l
v
1
8
.•~n
E
:
• 100
80:~
0 240~
•
120~ -~
I I
sov
' so<~
c Fig. 1.111 Copyrghlcd
nalcri~
Circuit Theory
1 -100 Bask; Circuit Analysis & Network Reduction Technlqun
21. Find tl!. cum:nt in
alii~!.
lml1u:hts
of II!. nd1vorl: shoum in II!. Fig. 1.112. tAns.: 39 A. n A. 39 A. 81 A. 11 A. 41 Al 80A
A
30A
80A
60A
70A
0
120A
Fig. 1.112 22.
If tht toW powu dissipaltd in II!. circuil sJrown in tht Fig.
1.113 is 18 Willis, foul tht zralue of R
and curmtl through it. 80
....
R
160
(ADs. : 12 a , 0.6 Al
40
,.
,.
+I , I'
12V
Fig. 1.113 23. The Comtnl in tJ1t 6
a rtsistmct qj IM nttwor/c sJrown in IM fig. 1.114 is 2 A. Ddnmint fht
curmds in all '"' other resulllnas and tht slq.ply t10114gt V. (Ana. : 1.5 A, l.5 A, 1 A. 46 V) 2A
HI
..••••'. 80
60
,..
AA AA.
.... 20h
y
8h' +
v Fig. 1.114
bllttay w1om w.uw by • resatance of so o gives tJre turni1W mu.ge of 48.6 v. If tht load resisl4n« is mcr-d to 100 a' tht ttrmhtal t10114ge is obsnwd to "" 49.2 v.
24. A parli&u!Rr
Copyrghtcd na
.ri~
Ci rcuit Theory
1 - 101 Basic Circuit Analysis & Network Reduction Techniques i) E.M.F. of ba!ttty
ii) lnttmal resistanct of batttty 25. A r..Utmlcr: of 10 0 is
26. Two storage ba!ltrits A and 8 an
27. A ntlwork ABCD is mode up as follaws :
A.B has • «
t terminal connected to II; BC is a r..Utor of 25 n ; CD is n resistor of 100 n ; DA is n batltty of 4 V and negligible r..UtDnce with po
S.j80
8-tj60
L-------L-----------~8
Fig. 1.115 (Ana.: 757 + j 157(1)
29. Find lht single vollllgt smiTe< equi'oaltnl across the ltrminals A·B. Hence obtain the single current $DUree equivalmt also. r------r---{:=}---~----~A
4+j3ll 3+j20
'
2~0V
2+j51l
~-----L----------~----~8
Fig. 1.116 (Ans.: V •10.78 Lts.06•V, Z • 1.66 + j 2.U!I;, I • 4 L-36.86' A)
000
Copyrgh!cd malcri~