Official Paper

GATE EE 2012 Official Paper (Previous Year Paper)

65 questions · 180 minutes · with answers · free

General Aptitude (10 questions)

1

One of the parts (A, B, C, D) in the sentence given below contains an ERROR. Which one of the following is INCORRECT?

I requested that he should be given the driving test today instead of tomorrow.

  1. ((a))

    requested that

  2. ((b))

    should be given

  3. ((c))

    the driving test

  4. ((d))

    instead of tomorrow

Show Answer
Answer: ((b))

should be given

The correct answer is 'should be given'; i.e. the error lies in this part of the sentence.

Key Points

  • The given sentence is in active voice which represents a form or set of forms of a verb in which the subject is typically the person or thing performing the action and which can take a direct object.
  • Thus, the usage of 'be given' is incorrect which is used with a passive voice which is used when we want to emphasize the action (the verb) and the object of a sentence rather than subject.
  • Thus, 'should be given' needs to be replaced with 'should give'.

Therefore, the correct sentence is: 'I requested that he should give the driving test today instead of tomorrow.'

2

If (1.001)1259 = 3.52 and (1.001)2062 = 7.85, then (1.001)3321 =

  1. ((a))

    2.23

  2. ((b))

    4.33

  3. ((c))

    11.37

  4. ((d))

    27.64

Show Answer
Answer: ((d))

27.64

Given:

(1.001)1259 = 3.52 and (1.001)2062 = 7.85

Concept used:

X(a + b) = X(a) × X(b)

Calculation:

⇒ (1.001)3321 = (1.001)1259 + 2062 

= (1.001)1259 × (1.001)2062

= 3.52 × 7.85

= 27.64

Hence, the correct answer is "27.64".

3

Choose the most appropriate alternative from the options given below to complete the following sentence:

If the tired soldier wanted to lie down, he _______ the mattress out on the balcony.

  1. ((a))

    should take

  2. ((b))

    shall take

  3. ((c))

    should have taken

  4. ((d))

    will have taken

Show Answer
Answer: ((c))

should have taken

The correct answer is 'should have taken'.

Key Points

  • Mixed Conditional Sentence: Mixed conditionals are conditional sentences that mix two different times in one sentence or we can say that the if-clause is not the same as the time in the result.
  • Structure for Mixed conditional (for present condition, past result):
  • If/when + past simple, would have + verb infinitive.
  • Example: 
  • If Sam spoke Russian, he would have translated the letter for you.
  • (But Sam doesn't speak Russian and that is why he didn't translate the letter.)
  • Note: Would can be replaced with should/might in the sentence.

Therefore, the correct sentence is: If the tired soldier wanted to lie down, he should have taken the mattress out on the balcony. 

Additional Information

  • Conditional sentence:- As the name suggests, these sentences express conditions.
  • In conditional sentences, there are two clauses of the sentences. One is a conditional clause and another one is main clause.
  • Other Conditional sentences are-
Types of Conditional SentencesDefinition and examples
Zero conditional SentenceIt expresses a factual condition.
Structure: If/When+ present simple+ present simple
Example: If you put ice in milk, It melts
First Conditional SentenceIt expresses possible and likely future outcomes.
Structure: If/when+present simple, will+ verb infinitive.
Example: If it's hot tomorrow, I'll go for a swim
Second Conditional SentenceIt expresses an Imagination.
Structure: If/when + past simple, would + verb infinitive.
Example: If I finished work earlier, I would leave.
Third Conditional sentenceIt expresses a hypothetical situation.
Structure: If/when+ past perfect+would have+ past participle.
Example: If I had been sick, I would have gone to the doctor
4

Choose the most appropriate word from the options given below to complete the following sentence:

Given the seriousness of the situation that he had to face, his _______ was impressive.

  1. ((a))

    beggary

  2. ((b))

    nomenclature

  3. ((c))

    jealousy

  4. ((d))

    nonchalance

Show Answer
Answer: ((d))

nonchalance

The correct answer is 'nonchalance'.

Key Points

  • Let's explore the options:
  • beggary: a state of extreme poverty.
  • Example: They have no benefits to stand between them and beggary.
  • nomenclature: the devising or choosing of names for things, especially in a science or other discipline.
  • Example: The Linnean system of zoological nomenclature
  • jealousy: the state or feeling of being jealous.
  • Example: He broke his brother's new bike in a fit of jealousy.
  • nonchalance: the trait of remaining calm and seeming not to care.
  • Example: He leaned back in his chair with apparent nonchalance.
  • Thus, from above we can refer that the correct answer is option 4.

Therefore, the correct sentence is: 'Given the seriousness of the situation that he had to face, his nonchalance was impressive.'

5

Which one of the following options is the closest in meaning to the word given below?

Latitude

  1. ((a))

    Eligibility

  2. ((b))

    Freedom

  3. ((c))

    Coercion

  4. ((d))

    Meticulousness

Show Answer
Answer: ((b))

Freedom

The correct answer is 'Freedom'.

Key Points

  • Latitude: scope for freedom of action or thought.
  • Example: Journalists have considerable latitude in criticizing public figures.
  • Freedom: the power or right to act, speak, or think as one wants without hindrance or restraint.
  • Example: We do have some freedom of choice.
  • Thus, the correct answer is option 2.

Additional Information

  • Let's explore options:
  • Eligibility: the state of having the right to do or obtain something through satisfaction of the appropriate conditions.
  • Coercion: the practice of persuading someone to do something by using force or threats.
  • Meticulousness: showing great attention to detail; very careful and precise.
6

A and B are friends. They decide to meet between 1 PM and 2 PM on a given day. There is a condition that whoever arrives first will not wait for the other for more than 15 minutes. The probability that they will meet on that day is

  1. ((a))

    1/4

  2. ((b))

    1/16

  3. ((c))

    7/16

  4. ((d))

    9/16

Show Answer
Answer: ((c))

7/16

A meeting occurs if the person arrives between 1:00 PM and 1:45 PM and the second person arrives in the next 15 minutes or if both the persons arrive between 1:45 and 2:00.

Case 1:

45/60 are favorable cases and hence the probability of first-person arriving between 1:00 and 1:45 is 3/4.

Probability of second person arriving in the next 15 min = 15/60 = 1/4

So, the probability of one person arriving between 1:00 and 1:45 and meeting the other = 3/4 × 1/4 × 2 = 3/8 (2 for choosing the first arriving friend)

Case 2: 

Both friends must arrive between 1:45 and 2:00

Probability = 1/4 × 1/4 = 1/16

So, probability of a meet = 3/8 + 1/16 = 7/16

Hence, the correct answer is 7/16.

7

One of the legacies of the Roman legions was discipline. In the legions, military law prevailed and discipline was brutal. Discipline on the battlefield kept units obedient, intact and fighting, even when the odds and conditions were against them.

Which one of the following statements best sums up the meaning of the above passage?

  1. ((a))

    Thorough regimentation was the main reason for the efficiency of the Roman legions even in adverse circumstances.

  2. ((b))

    The legions were treated inhumanly as if the men were animals.

  3. ((c))

    Discipline was the armies’ inheritance from their seniors.

  4. ((d))

    The harsh discipline to which the legions were subjected to led to the odds and conditions being against them.

Show Answer
Answer: ((a))

Thorough regimentation was the main reason for the efficiency of the Roman legions even in adverse circumstances.

The correct answer is 'Thorough regimentation was the main reason for the efficiency of the Roman legions even in adverse circumstances.'

Key Points

  • Let's refer to the following lines of the passage:
  • In the legions, military law prevailed and discipline was brutal. Discipline on the battlefield kept units obedient, intact and fighting, even when the odds and conditions were against them.
  • Thus, from above we can infer that the correct answer is option 1.

Additional Information

  • Regimentation: organize according to a strict system or pattern.
8

Raju has 14 currency notes in his pocket consisting of only Rs. 20 notes and Rs. 10 notes. The total money value of the notes is Rs. 230. The number of Rs. 10 notes that Raju has is

  1. ((a))

    5

  2. ((b))

    6

  3. ((c))

    9

  4. ((d))

    10

Show Answer
Answer: ((a))

5

Let's consider number of 10 rupee notes as 'x'

And number of 20 rupees notes as 'y'

Then total number of notes = x + y = 14 -------(1)

Total money = 10x + 20y = 230  ---------(2)

By solving (1) and (2), we get

x = 5 and y = 9

9

There are eight bags of rice looking alike, seven of which have equal weight and one is slightly heavier. The weighing balance is of unlimited capacity. Using this balance, the minimum number of weighings required to identify the heavier bag is

  1. ((a))

    2

  2. ((b))

    3

  3. ((c))

    4

  4. ((d))

    8

Show Answer
Answer: ((a))

2

Explanation:

Divide 8 bags into three parts.

2,2 and 4 respectively.

If we compare the 2,2 bags on pans of a balance.

We can identify which side is the lighter bag placed.

And then we will need only one more weighing for identifying the faulty bag.

So only two weighings are required.

Alternative solution:

In the case of a weighing balance (i.e. beam balance) the following model can be observed.

1 - 3 → 1 weighing required

4 - 9 → 2 weighings required

10 - 27 → 3 weighings required

28 - 81 → 4 weighings required

And the process will go so on.

As there are eight objects. The minimum number of weighings required will be only 2.

10

The data given in the following table summarizes the monthly budget of an average household

CategoryAmount (Rs.)
Food4000
Clothing1200
Rent2000
Savings1500
Other expenses1800
<br>

The approximate percentage of the monthly budget NOT spent on savings is

  1. ((a))

    10%

  2. ((b))

    14%

  3. ((c))

    81%

  4. ((d))

    86%

Show Answer
Answer: ((d))

86%

Total budget = 10500 Rs

Expenditure  other than savings = 9000

The approximate percentage of the monthly budget NOT spent on savings is = (9000/ 10500) × 100

= 85.71 % ≈ 86%

Electrical Engineering (55 questions)

11

Two independent random variables X and Y are uniformly distributed in the interval [–1,1]. The probability that max[X, Y] is less than 1/2 is

  1. ((a))

    3/4

  2. ((b))

    9/16

  3. ((c))

    1/4

  4. ((d))

    2/3

Show Answer
Answer: ((b))

9/16

P(max(X,Y) < .5) = P(X <.5, Y < 0.5)

Since X and Y are independent random variable, therefore

P(X <.5, Y < 0.5) = P(X < .5) P(Y < .5)

X and Y are uniformly distributed in [-1,1]

PDF of X and Y are

Thus,

P(X > 2) P(Y > 2)

12

If x = √-1, then the value of xx is

  1. ((a))

    e-π/2

  2. ((b))

    eπ/2

  3. ((c))

    x

  4. ((d))

    1

Show Answer
Answer: ((a))

e-π/2

Let A = xx

Taking logarithm both the sides.

Log A = x log x = i log (0 + x)

As |x| = 1 and arg (x) = π/2,

Log A = x(log1 + xπ/2) = x(0 + x π/2)

Log A = -π/2

Hence, A = e- π/2

13

Given f(z)=1z+12z+3f(z)=\frac{1}{z+1}-\frac{2}{z+3}. If C is a counterclockwise path in the z-plane such that |z + 1| = 1, the value of 12πicf(z)dz\frac{1}{2\pi i}\int_c f(z)dz is

  1. ((a))

    -2

  2. ((b))

    -1

  3. ((c))

    1

  4. ((d))

    2

Show Answer
Answer: ((c))

1

f(z);=;1z+12z+3;=;z+1(z+1)(z+3)f\left( z \right); = ;\frac{1}{{z + 1}} - \frac{2}{{z + 3}}; = ;\frac{{ - z + 1}}{{\left( {z + 1} \right)\left( {z +3} \right)}}

The poles of f(z) are - 1 and -3 and -3 is outside of the circle |z + 1| = 1.

By Cauchy’s formula,

f(z)zadz;=;2πif(a) z+1(z+3)(z+1)dz;=;z+1(z+3)(z+1)dz\begin{array}{l} \smallint \frac{{f\left( z \right)}}{{z - a}}dz; = ;2\pi if\left( a \right)\ \smallint \frac{{ - z + 1}}{{\left( {z + 3} \right)\left( {z +1} \right)}}dz; = ;\smallint \frac{{\frac{{ - z +1}}{{\left( {z +3} \right)}}}}{{\left( {z + 1} \right)}}dz \end{array}

By Cauchy’s formula,

;2πif(1);=;2πi((1)+11+3);=;2πi ;12πif(z)dz;=;1\begin{array}{l} \Rightarrow ;2\pi if\left( { - 1} \right); = ;2\pi i\left( {\frac{{-(-1) + 1}}{{ - 1 + 3}}} \right); = ;2\pi i\ \Rightarrow ;\frac{1}{{2\pi i}}\smallint f\left( z \right)dz; = ;1 \end{array}

14

In the circuit shown below, the current through the inductor is

  1. ((a))

    21+jA\frac{2}{{1 + j}}A

  2. ((b))

    11+jA\frac{{ - 1}}{{1 + j}}A

  3. ((c))

    11+jA\frac{1}{{1 + j}}A

  4. ((d))

    0 A

Show Answer
Answer: ((c))

11+jA\frac{1}{{1 + j}}A

Applying nodal analysis at top node

V1+101+V1+10j1=10\frac{{{V_1} + 1\angle 0^\circ }}{1} + \frac{{{V_1} + 1\angle 0^\circ }}{{j1}} = 1\angle 0^\circ

V1 = (j1 + 1) + j1 + 1 ∠ 0° = j1

V1=11+j1 I1=V1=V1+10j1=1j+1+1j1=j(1+j)j=1(1+j)A\begin{array}{l} {V_1} = \frac{{ - 1}}{{1 + j1}}\ {I_1} = {V_1} = \frac{{{V_1} + 1\angle 0^\circ }}{{j1}} = \frac{{\frac{{ - 1}}{{j + 1}} + 1}}{{j1}} = \frac{j}{{\left( {1 + j} \right)j}} = \frac{1}{{\left( {1 + j} \right)}}A \end{array}

15

The impedance looking into nodes 1 and 2 in the given circuit is

  1. ((a))

    50 Ω

  2. ((b))

    100 Ω

  3. ((c))

    5 KΩ

  4. ((d))

    10.1 KΩ

Show Answer
Answer: ((a))

50 Ω

Assume a voltage source V between 1 and 2 ,

then VI=impendance\frac{V}{I} = impendance at 1 and 2

ib=0V10 KΩ{i_b} = \frac{{0 - V}}{{10\ K{\rm{\Omega }}}}         ___________(1)

Apply Nodal analysis then

ib+V10099ibI=0- {i_b} + \frac{V}{{100}} - 99{i_b} - I = 0

V = 104 ib + 100 I        ___________(2)

From (1) and (2) we get

V=104(V104)+100 IV = {10^4}\left( {\frac{{ - V}}{{{{10}^4}}}} \right) + 100\ I

2V = 100 I

Impendence =VI=50 Ω= \frac{V}{I} = 50\ {\rm{\Omega }}

∴ Option (1) is correct

16

A system transfer function

G(s)=(s2+9)(s+2)(s+1)(s+3)(s+4)G\left( s \right) = \frac{{\left( {{s^2} + 9} \right)\left( {s + 2} \right)}}{{\left( {s + 1} \right)\left( {s + 3} \right)\left( {s + 4} \right)}}

is excited by sin(ωt). The steady state output of system is zero at

  1. ((a))

    ω = 1 rad/sec

  2. ((b))

    ω = 3 rad/sec

  3. ((c))

    ω = 2 rad/sec

  4. ((d))

    ω = 4 rad/sec

Show Answer
Answer: ((b))

ω = 3 rad/sec

;sinωtG(s)Y(s)=G(s)sin(ωt+G(s));\sin \omega t \to \boxed{G\left( s \right)} \to Y\left( s \right) = \left| {G\left( s \right)} \right| \cdot \sin \left( {\omega t + \angle G\left( s \right)} \right)

Output will be zero when

|G(s)| = 0

Put s = jω

(ω2+9)(jω+2)(jω+1)(jω+3)(jω+4)=0\left| {\frac{{\left( { - {\omega ^2} + 9} \right)\left( {j\omega + 2} \right)}}{{\left( {j\omega + 1} \right)\left( {j\omega + 3} \right)\left( {j\omega + 4} \right)}}} \right| = 0

at         ω = 3   , |G(jω)| = 0

17

In the sum of products function f (X, Y, Z) = ∑ (2, 3, 4, 5) , the prime implicants are

  1. ((a))

    X̅Y, XY̅

  2. ((b))

    X̅Y, XY̅Z̅, XY̅Z

  3. ((c))

    X̅YZ̅, X̅YZ, XY̅

  4. ((d))

    X̅YZ̅, X̅YZ, XY̅Z̅, XY̅Z

Show Answer
Answer: ((a))

X̅Y, XY̅

Prime implicant is a minterm, which are obtained by combining maximum possible adjacent cell in k-map

F(x,y,z)=xˉyˉ+xyF\left( {x,y,z} \right) = \bar x\bar y + xy

18

If x[n] = (1/3)|n| - (1/2)n u[n], then the region of convergence (ROC) of its z-transforms in the z-plane will be

  1. ((a))

    z>3\left| z \right| > 3

  2. ((b))

    13<z<12\frac{1}{3} < \left| z \right| < \frac{1}{2}

  3. ((c))

    12<z<3\frac{1}{2} < \left| z \right| < 3

  4. ((d))

    13<z\frac{1}{3} < \left| z \right|

Show Answer
Answer: ((c))

12<z<3\frac{1}{2} < \left| z \right| < 3

x[n]=(13)n(12)nu[n] =(13)nu[n]+(13)n1u[n1](12)nu[n]\begin{array}{l} x\left[ n \right] = {\left( {\frac{1}{3}} \right)^{\left| n \right|}} - {\left( {\frac{1}{2}} \right)^n}u\left[ n \right]\ = {\left( {\frac{1}{3}} \right)^n}u\left[ n \right] + {\left( {\frac{1}{3}} \right)^{n - 1}}u\left[ { - n - 1} \right] - {\left( {\frac{1}{2}} \right)^n}u\left[ n \right] \end{array}

Taking Z-transform

\(\begin{array}{l} X\left[ z \right] = \mathop \sum \limits_{n = - \infty }^\infty {\left( {\frac{1}{3}} \right)^n}{z^{ - n}}u\left[ n \right] + \mathop \sum \limits_{n = - \infty }^\infty {\left( {\frac{1}{3}} \right)^{ - n}}{z^{ - n}}u\left[ { - n - 1} \right] - \mathop \sum \limits_{n = - \infty }^\infty {\left( {\frac{1}{2}} \right)^n}{z^{ - n}}u\left[ n \right]\ = \mathop \sum \limits_{n = 0}^\infty {\left( {\frac{1}{3}} \right)^n}{z^{ - n}} + \mathop \sum \limits_{n = - \infty }^{ - 1} {\left( {\frac{1}{3}} \right)^{ - n}}{z^{ - n}} - \mathop \sum \limits_{n = 0}^\infty {\left( {\frac{1}{2}} \right)^n}{z^{ - n}}\ = \underbrace {\mathop \sum \limits_{n = 0}^\infty {{\left( {\frac{1}{{3Z}}} \right)}^n}}I + \underbrace {\mathop \sum \limits{m = 1}^\infty {{\left( {\frac{Z}{3}} \right)}^m}}{II} - \underbrace {\mathop \sum \limits{n = 0}^\infty {{\left( {\frac{1}{{2Z}}} \right)}^n}}_{III} \end{array}\)

Series I converges if 13Z<1orZ>13\left| {\frac{1}{{3Z}}} \right| < 1or\left| Z \right| > \frac{1}{3}

Series II converges if 13z<1 or Z<3\left| {\frac{1}{3}z} \right| < 1\ or\ \left| Z \right| < 3

Series III converges if 12Z<1 or Z>12\left| {\frac{1}{{2Z}}} \right| < 1\ or\ \left| Z \right| > \frac{1}{2}

Region of convergence of X(Z) will be intersection of above three

So, ROC  12<Z<3\frac{1}{2}< |Z| < 3.

19

The bus admittance matrix of a three – bus three – line system is

\(Y = j\left[ {\begin{array}{*{20}{c}} { - 13}&{10}&5\ {10}&{ - 18}&{10}\ 5&{10}&{ - 13} \end{array}} \right]\)

If each transmission line between the two buses is represented by an equivalent π – network, the magnitude of the shunt susceptance of the line connecting bus 1 and 2 is

  1. ((a))

    4

  2. ((b))

    2

  3. ((c))

    1

  4. ((d))

    0

Show Answer
Answer: ((b))

2

Concept:

Bus Admittance Matrix:

  • In a power system, Bus Admittance Matrix represents the nodal admittances of the various buses.
  • Admittance matrix is used to analyze the data that is needed in the load or a power flow study of the buses.
  • It explains the admittance and the topology of the network.
<br>

In a y-bus matrix,

The diagonal element Yii is the sum of all the admittances of the elements connected to the ith bus.

Yii = Σ yik , k = 1, 2, …n and k ≠ i

The off-diagonal element Yij is equal to the minus of the admittance of the element connected between buses i and j.

Yij = -yij

Application:

From the above concept,

Y22 = Y21 + Y22 + Y23

Y21 = -y21, y23 = -y23

From the given Y bus matrix \(Y = j\left[ {\begin{array}{*{20}{c}} { - 13}&{10}&5\ {10}&{ - 18}&{10}\ 5&{10}&{ - 13} \end{array}} \right]\)

Y22 = -18, Y21 = 10, Y23 = 10

Y21 = -y21

Y23 = -y23

Y22 = y21 + y22 + y23

-18j = (-10j) + y22 + (-10j) ⇒ y22 = 2j

similarly, y11 = y33 = 2j

Here 2j is shunt capacitance at each bus divides into half in π model at

the buses located

Therefore,the system looks like

y11 = y01 + y01 = 2 y01

2j = 2 y01

y01 = j

similarly, y02 = j

The magnitude of the shunt susceptance of the line connecting bus

1 and 2 is y01 + y02

j + j = 2j Ω

20

The slip of an induction motor normally does not depend on: 

  1. ((a))

    Rotor speed 

  2. ((b))

    Synchronous speed

  3. ((c))

    Shaft torque

  4. ((d))

    Core-loss component

Show Answer
Answer: ((d))

Core-loss component

The slip of an induction motor is given by,

s=NsNrNs×100s = \frac{{{N_s} - {N_r}}}{{{N_s}}} \times 100

It directly depends on rotor speed and synchronous speed. It is indirectly depends on shaft torque but it is independent of core loss component.

21

A Two – phase load draws the following phase currents: i1(t)=Imsin(ωtϕ1),i2(t)=Imcos(ωtϕ2){i_1}\left( t \right) = {I_m}\sin \left( {\omega t - {\phi _1}} \right),{i_2}\left( t \right) = {I_m}\cos \left( {\omega t - {\phi _2}} \right) These currents are balanced if ϕ1 {\phi _1} is equal to

  1. ((a))

    ϕ2- {\phi _2}

  2. ((b))

    ϕ2 {\phi _2}

  3. ((c))

    (π2ϕ2)\left( {\frac{\pi }{2} - {\phi _2}} \right)

  4. ((d))

    (π2+ϕ2)\left( {\frac{\pi }{2} + {\phi _2}} \right)

Show Answer
Answer: ((b))

ϕ2 {\phi _2}

Given that,

i1(t)=Imsin(ωtϕ1),i2(t)=Imcos(ωtϕ2){i_1}\left( t \right) = {I_m}\sin \left( {\omega t - {ϕ _1}} \right),{i_2}\left( t \right) = {I_m}\cos \left( {\omega t - {ϕ _2}} \right)

If these currents are balanced,

The angle between i1(t) and i2(t) should be 90°

90° = ϕ2 + 90 - ϕ1

∴ ϕ1 = ϕ2

22

A periodic voltage waveform observed on an oscilloscope across a load is shown. A permanent magnet moving coil (PMMC) meter connected across the same load reads

  1. ((a))

    4 V

  2. ((b))

    5 V

  3. ((c))

    8 V

  4. ((d))

    10 V

Show Answer
Answer: ((a))

4 V

Concept:

The DC value or the average value of a waveform f(t) is given by the Area under the curve for one complete time period; i.e.,

\({f_{DC}} = \frac{1}{T}\mathop \smallint \nolimits_o^T f\left( t \right)dt\)

RMS value 'or' the effective value of an alternating quantity is calculated as:

\({V_{rms}} = \sqrt{\frac{1}{T}\mathop \smallint \limits_0^T {v^2}\left( t \right)dt} \)

Calculation:

Average value,

\(\begin{array}{l} = \frac{1}{{20}}\left[ {\mathop \smallint \limits_0^{10} tdt - \mathop \smallint \limits_{10}^{12} 5dt + \mathop \smallint \limits_{12}^{20} 5dt} \right]\ = {\rm{ }}4\ {\rm{ }}V \end{array}\)

23

Among the following which one of the bridge method is commonly used for finding mutual inductance

  1. ((a))

    Wein Bridge

  2. ((b))

    Schering Bridge 

  3. ((c))

    De Sauty Bridge 

  4. ((d))

    Heaviside Campbell Bridge 

Show Answer
Answer: ((d))

Heaviside Campbell Bridge 

Heaviside bridge:

  • Heaviside bridge is used to measure the mutual inductance.
  • The bridge which measures the unknown mutual inductance regarding mutual inductance such type of bridge is known as the Campbell bridge.
  • Mutual inductance is the phenomenon in which the variation of current in one coil induces the current in the nearer coil.
  • The bridge also used for measuring the frequency by adjusting the mutual inductance until the null point is not obtained.

Important Points

Type of BridgeName of BridgeUsed to measureImportant
DC BridgesWheatstone bridgeMedium resistance
Corey foster’s bridgeMedium resistance
Kelvin double bridgeVery low resistance
Loss of charge methodHigh resistance
MeggerHigh insulation resistanceResistance of cables
AC BridgesMaxwell’s inductance bridgeInductanceNot suitable to measure Q
Maxwell’s inductance capacitance bridgeInductanceSuitable for medium Q coil (1 < Q < 10)
Hay’s bridgeInductanceSuitable for high Q coil (Q > 10), slowest bridge
Anderson’s bridgeInductance5-point bridge, accurate and fastest bridge (Q < 1)
Owen’s bridgeInductanceUsed for measuring low Q coils
Heaviside mutual inductance bridgeMutual inductance
Campbell’s modification of Heaviside bridgeMutual inductance
De-Sauty’s bridgeCapacitanceSuitable for perfect capacitor
Schering bridgeCapacitanceUsed to measure relative permittivity
Wein’s bridgeCapacitance and frequencyHarmonic distortion analyzer, used as a notch filter, used in audio and high-frequency applications
24

With initial condition x(1) = 0.5 , the solution of the differential equation tdxdt+x=tt\frac{dx}{dt}+x=t is

  1. ((a))

    x=t12x=t-\frac{1}{2}

  2. ((b))

    x=t212x=t^2-\frac{1}{2}

  3. ((c))

    x=t22x=\frac{t^2}{2}

  4. ((d))

    x=t2x=\frac{t}{2}

Show Answer
Answer: ((d))

x=t2x=\frac{t}{2}

Given differential equation is tdxdt+x;=;tt\frac{{dx}}{{dt}} + x; = ;{t}

;dxdt+1tx;=;1\Rightarrow ;\frac{{dx}}{{dt}} + \frac{1}{t}x; = ;1

This is a linear differential equation in t.

I.F.;=;e1tdt;=;elogt;=;tI.F.; = ;{e^{\smallint \frac{1}{t}dt}}; = ;{e^{\log t}}; = ;t

The solution is,

x.(IF);=;1.(IF)dt+cx.t;=;tdt+c ;xt;=;t22+c\begin{array}{l} x.(IF); = ;\smallint 1.(IF)dt + c\Rightarrow x.t; = ;\smallint tdt + c\ \Rightarrow ;xt; = ;\frac{{{t^2}}}{2} + c \end{array}

Given x(1) = .5 ⇒ c = 0

The solution is x;=;t2x; = ;\frac{{{t}}}{2}

25

The unilateral Laplace transform of f(t) is 1s2+s+1\frac{1}{s^2+s+1}. The unilateral Laplace transform of t f(t) is

  1. ((a))

    s(s2+s+1)2-\frac{s}{(s^2+s+1)^2}

  2. ((b))

    2s+1(s2+s+1)2-\frac{2s+1}{(s^2+s+1)^2}

  3. ((c))

    s(s2+s+1)2\frac{s}{(s^2+s+1)^2}

  4. ((d))

    2s+1(s2+s+1)2\frac{2s+1}{(s^2+s+1)^2}

Show Answer
Answer: ((d))

2s+1(s2+s+1)2\frac{2s+1}{(s^2+s+1)^2}

Concept

Multiplication of function in one domain corresponds to the differentiation in another domain

If f(t) having the Laplace transform F(s) then t ⋅ f(t) will have the transform as

  t f(t) ↔dF(s)ds - \frac{{dF\left( s \right)}}{{ds}}

Calculation:

Given function f(t) is . And  g(t) = t ⋅ f(t)

Laplace transform of g(t) is:

L[g(t)]=dds(1s2s+1)L[g(t)] = - \frac{d}{{ds}}\left( {\frac{1}{{{s^2}s + 1}}} \right)

=d(1)ds(s2+s+1)1×d(S2+S+1)ds(S2+S+1)2 = - \frac{{\frac{{d\left( 1 \right)}}{{ds}}\left( {{s^2} + s + 1} \right) - 1 \times \frac{{d\left( {{S^2} + S + 1} \right)}}{{ds}}}}{{{{\left( {{S^2} + S + 1} \right)}^2}}}

=(01(2s+1)(s2+s+1)2) = - \left( {\frac{{0 - 1\left( {2s + 1} \right)}}{{{{\left( {{s^2} + s + 1} \right)}^2}}}} \right)

=2s+1(s2+s+1)2 = \frac{{2s + 1}}{{{{\left( {{s^2} + s + 1} \right)}^2}}}

26

The average power delivered to an impedance (4 – j3) Ω by a current 5 cos (100πt + 100) A is

  1. ((a))

    44.2 W

  2. ((b))

    50 W

  3. ((c))

    62.5 W

  4. ((d))

    125 W

Show Answer
Answer: ((b))

50 W

In phasor form:

Z = 4 – j3

Z = 5 ∠-36.86° Ω

I = 5 ∠100° A

Average power delivered will be:

Pavg=12I2Zcosθ%MathType!End!2!1!{P_{avg}} = \frac{1}{2}{\left| I \right|^2}Zcos\theta \% MathType!End!2!1!

= (½) × 25 × 5 cos 36.86°

= 50 W

Alternate Approach:

The power delivered to the load will simply be the power dissipated by the resistor R, i.e.

Pdelivered = IRMS2 R

With Im = 5, IRMS will be:

IRMS=52I_{RMS} = \frac{5}{\sqrt 2}

Pdelivered=(52)2×4P_{delivered} = (\frac{5}{\sqrt 2})^2\times 4

Pdelivered=252×4=50 WP_{delivered} =\frac{25}{2}\times 4 = 50~W

27

In the following figure, C1 and C2 are ideal capacitors. C1 has been charged to 12 V before the ideal switch S is closed at t = 0. The current i(t) for all t is

  1. ((a))

    Zero

  2. ((b))

    A step function

  3. ((c))

    An exponentially decaying function

  4. ((d))

    An impulse function

Show Answer
Answer: ((d))

An impulse function

The S – domain equivalent circuit is

I(S)=Vc(0)S1C1S+1C2S=Vc(0)(1C1+1C2)%MathType!End!2!1! I\left( S \right) = \frac{{\frac{{{V_c}\left( 0 \right)}}{S}}}{{\frac{1}{{{C_1}S}} + \frac{1}{{{C_2}S}}}} = \frac{{{V_c}\left( 0 \right)}}{{\left( {\frac{1}{{{C_1}}} + \frac{1}{{{C_2}}}} \right)}}\% MathType!End!2!1!

Vc(0) = 12 V

I(S)=(C1C2C1+C2)(12)%MathType!End!2!1!I\left( S \right) = \left( {\frac{{{C_1}{C_2}}}{{{C_1} + {C_2}}}} \right)\left( {12} \right)\% MathType!End!2!1!

I(S) = 12 Ceq

Taking Inverse Laplace transform for the current in the time domain.

i(t) = 12 Ceq δ(t) 

The above equation shows that it's an impulse.

28

The i-v characteristics of the diode in the circuit given below are

\(i= \left{ \begin{matrix} \frac{v-0.7}{500}A && v \ge 0.7 V \\ 0 A && v < 0.7 V \end{matrix}\right.\)

The current in the circuit is

  1. ((a))

    10 mA

  2. ((b))

    9.3 mA

  3. ((c))

    6.67 mA

  4. ((d))

    6.2 mA

Show Answer
Answer: ((d))

6.2 mA

Let's consider v >.7 and the diode is forward biased. 

By applying KVL, we get

10 - I × 1k - v = 0

10 -[(v-.7)/(500)] × 1000 - v = 0

⇒ v = 3.8 V 

And v > .7 and our assumption is correct,

i =[(v-.7)/(500)] = [3.8 - 0.7]/500 = 6.2 mA

29

The output Y of a 2-bit comparator is logic 1 whenever the 2-bit input A is greater than the 2-bit input B. The number of combinations for which the output is logic 1, is

  1. ((a))

    4

  2. ((b))

    6

  3. ((c))

    8

  4. ((d))

    10

Show Answer
Answer: ((b))

6

The only possible combinations are

A = 01 and B = 0 0

A = 10 and B = 00, 01

A = 11 and B = 00, 01, 10

So there are only 6 combinations

Tips and Tricks:

22n2n2\frac{2^{2n} - 2^n}{2}

where n = 2 bit

30

Consider the given circuit. In this circuit, the race around

  1. ((a))

    Does not occur

  2. ((b))

    Occurs when CLK = 0

  3. ((c))

    Occurs when CLK = 1 and A = B = 1

  4. ((d))

    Occurs when CLK = 1 and A = B = 0

Show Answer
Answer: ((a))

Does not occur

The circuit is a SR flip-flop with input A = S and B = R. In SR flip-flop there is no race around condition for any combination of input.

Note :

11 is a not allowed state because the output Q and Q'  will be 1. 

For race around Q should toggle.

It occurs in JK flip flop when J=K=1 and there is unequal propagation delay.

31

The figure shows a two – generator system applying a load of PD = 40 MW, connected at bus 2.

The fuel cost of generators G1 and G2 are :

C1(PG1) = 10000 Rs/MWh and C2(PG2) = 12500 Rs/MWh and the loss in the line is

 Ploss(Pu)=0.5PG1(Pu)2{P_{loss\left( {Pu} \right)}} = 0.5P_{G1\left( {Pu} \right)}^2, Where the loss coefficient is specified in pu on a 100 MVA base. The most economic power generation schedule in MW is

  1. ((a))

    PG1 = 20, PG2 = 22

  2. ((b))

    PG1 = 22, PG2 = 20

  3. ((c))

    PG1 = 20, PG2 = 20

  4. ((d))

    PG1 = 0, PG2 = 40

Show Answer
Answer: ((a))

PG1 = 20, PG2 = 22

For economic load dispatch,

L1dF1dPG1=L2dF2dPG2 11dPLdPG1dF1dP1=11dPLdPG2dF2dP2\begin{array}{l} {L_1}\frac{{d{F_1}}}{{d{P_{G1}}}} = {L_2}\frac{{d{F_2}}}{{d{P_{G2}}}}\ \frac{1}{{1 - \frac{{d{P_L}}}{{d{P_{G1}}}}}}\frac{{d{F_1}}}{{d{P_1}}} = \frac{1}{{1 - \frac{{d{P_L}}}{{d{P_{G2}}}}}}\frac{{d{F_2}}}{{d{P_2}}} \end{array}

From the given data

dPLdP1=2(0.5)PF=PG1\frac{{d{P_L}}}{{d{P_1}}} = 2\left( {0.5} \right){P_F} = {P_{G1}} and

dPLdPG2=0 1(1PG1)×10000=1(10)×12500 (1PG1)=100125\begin{array}{l} \frac{{d{P_L}}}{{d{P_{G2}}}} = 0\ \frac{1}{{\left( {1 - {P_{G1}}} \right)}} × 10000 = \frac{1}{{\left( {1 - 0} \right)}} × 12500\ \left( {1 - {P_{G1}}} \right) = \frac{{100}}{{125}} \end{array}

1-PG1 = 0.8 ⇒ PG1 = 0.2 pu

⇒  PG1 = 0.2 × 100 = 20 MW

But PL=0.5P12{P_L} = 0.5P_1^2 

= 0.5 (0.2)2

PL = 0.02 Pu = .02 × 100 = 2 MW

PL is 10% PG1

PG1 + PG2 = PD + PL

⇒ 20 + PG2  = 40 + 2 

PG2 = 22 MW

32

The sequence components of the fault current are as follows: Ipositive = j 1.5 pu, Inegative = - j 0.5 pu, Izero = -j1pu. The type of fault in the system is

  1. ((a))

    LG

  2. ((b))

    LL

  3. ((c))

    LLG

  4. ((d))

    LLLG

Show Answer
Answer: ((c))

LLG

Concept:

In a single line to ground fault, all the sequence components of fault currents are equal.

Ia1 = Ia2 = Ia0

In a double line to ground fault, the sum of all sequence components of fault currents is zero.

Ia1 + Ia2 + Ia0 = 0

Where, Ia1 = Positive sequence component of the current

Ia2 = Negative sequence component of the current

Ia0 = Zero sequence component of the current

Calculation:

Given

Ipositive = j 1.5 p.u. 

Inegative = - j 0.5 p.u. 

Izero = - j 1 p.u.

Ia1 = j 1.5, Ia2 = -j 0.5, Ia0 = -j 1.0

⇒ Ia1 + Ia2 + Ia0 = j 1.5 – j 0.5 – j 1.0 = 0

Therefore, the fault is double line to ground fault.

33

A half controlled single phase bridge rectifier is supplying on R-L load. If it is operated at a firing angle α and the load current is continuous. The fraction of the cycle freewheeling diode conducts is

  1. ((a))

    12\frac{1}{2}

  2. ((b))

    (1απ)\left( {1 - \frac{\alpha }{\pi }} \right)

  3. ((c))

    α2π\frac{\alpha }{{2\pi }}

  4. ((d))

    απ\frac{\alpha }{\pi }

Show Answer
Answer: ((d))

απ\frac{\alpha }{\pi }

Answer:-

Fraction of conduction time freewheeling diode conducts

= α /π

Concept:- 

Circuit of single phase half controlled bridge rectifier is supplying on R-L load and Freewheeling diode.

  • The circuit consists of a thyristor T, voltage source Vs , a freewheeling diode across the RL load, an inductive load L and resistive load R.
  • During the positive half cycle of input voltage, the thyristor T is forward biased but it does not conduct until a gate signal is applied to it.
  • When the gate pulse is given to thyristor T, it gets turned on and begins to conduct.
  • When the thyristor is on, the input voltage is applied to the load but due to the inductor  present in the load, the current through the load build up slowly.
  • During the negative half cycle, the thyristor T gets reverse biased. At this instant i.e. at ωt=;π\omega t = ;\pi , the load current shift its path from the thyristor to the freewheeling diode.
  • When the current is shifted from thyristor to freewheeling diode, the thyristor turns off.( Fig.2)
  • The current through the inductor slowly decays to zero through the loop R – Freewheeling diode – L.
  • So here the thyristor will not conduct in the negative half cycle and turns off at α\alpha
  • So the load reverse voltage only during the positive half cycle.
  • The average value of output voltage can be varied by varying the firing angle

  • The waveform of voltage and current.

The Advantages of using Freewheeling Diode:-

  • It prevents the output voltage from becoming negative.
  • As the energy stored in the L is transferred to load R through freewheeling diode, the system efficiency is improved.
  • The load current waveform is more smooth.
  • The power factor is improved.
  • The performance of converter is improved with a freewheeling diode.
34

The typical ratio of latching current to holding current in a 20 A thyristor is

  1. ((a))

    5.0

  2. ((b))

    2.0

  3. ((c))

    1.0

  4. ((d))

    0.5

Show Answer
Answer: ((b))

2.0

Latching Current: It is the minimum anode current required to maintain the Thyristor in the ON state immediately after a Thyristor has been turned on and the gate signal has been removed.

Holding Current: It is the minimum anode current to maintain the Thyristor in the on-state.

  • Latching current is always greater than holding current.
  • Latching current and holding current terms have their significance in making a Thyristor ON and OFF respectively.
  • Thyristor goes to on state when Thyristor current is more than latching current.
  • Once Thyristor gets ON then there is no meaning of latching current.
  • For 20A Thyristor we have to use BT152 and the ratio of latching current to holding current in BT152  is in the range of 2.
35

For the circuit shown in the figure, the voltage and current expressions are

v(t) = E1sin(ωt) + E3sin(3ωt) and i(t) = I1sin(ωt - Φ1) + I3sin(3ωt - Φ3) + I5sin(5ωt)

The average power measured by the Wattmeter is

  1. ((a))

    12E1I1cosϕ1\frac{1}{2}E_1I_1cos\phi_1

  2. ((b))

    12[E1I1cosϕ1+E1I3cosϕ3+E1I5]\frac{1}{2}[E_1I_1cos\phi_1+E_1I_3cos\phi_3+E_1I_5]

  3. ((c))

    12[E1I1cosϕ1+E3I3cosϕ3]\frac{1}{2}[E_1I_1cos\phi_1+E_3I_3cos\phi_3]

  4. ((d))

    12[E1I1cosϕ1+E3I1cosϕ1]\frac{1}{2}[E_1I_1cos\phi_1+E_3I_1cos\phi_1]

Show Answer
Answer: ((c))

12[E1I1cosϕ1+E3I3cosϕ3]\frac{1}{2}[E_1I_1cos\phi_1+E_3I_3cos\phi_3]

Given that,

v(t) = E1sin(ωt) + E3sin(3ωt)

i(t) = I1sin(ωt - Φ1) + I3sin(3ωt - Φ3) + I5sin(5ωt)

As the 5th harmonic is not part of voltage expression, in the instantaneous power expression also we will have fundamental and third harmonic only.

p(t) = v(t) . i(t)

As wattmeter measures average power, it is given by

P = \(\frac{1}{2\pi}\mathop \smallint \limits_{0}^{2\pi} v(t).i(t) d \omega t\)     ------(1)

We know that,

\(\frac{1}{2\pi}\mathop \smallint \limits_{0}^{2\pi} A sin(\theta+\alpha).Bsin(\theta+\beta) d \theta=\frac{1}{2}ABcos(\alpha-\beta)\) -------(2)

By the use of the above result, if solve equation (1), we get

P = 12[E1I1cosϕ1+E3I3cosϕ3]\frac{1}{2}[E_1I_1cos\phi_1+E_3I_3cos\phi_3]

36

Given that

A=[5320]:and:I=[1001]A=\left[ \begin{matrix} -5 && -3 \\ 2 && 0 \end{matrix} \right] :and:I=\left[ \begin{matrix} 1 && 0 \\ 0 && 1 \end{matrix} \right] the value of A3 is

  1. ((a))

    15A + 12I

  2. ((b))

    19A + 30I

  3. ((c))

    17A + 15I

  4. ((d))

    17A + 21I

Show Answer
Answer: ((b))

19A + 30I

Concept:

  • Cayley - Hamilton theorem states that every square matrix A satisfies its own characteristic equation. i.e. p(A) = 0.
  • The characteristic polynomial of a matrix A is defined as: p(λ) = |λI - A|.
  • Identity Matrix:

An identity matrix is a matrix in which the diagonal elements are 1 and all the other elements are 0.

A 3×3 identity matrix is I = \(\rm \begin{bmatrix} 1 & 0 & 0 \0 & 1 & 0 \0 & 0 & 1 \end{bmatrix}\).

Matrix Multiplication by an Identity matrix results in the same matrix.

 

Calculation:

Let us find the characteristic polynomial p(λ) of the given matrix A = [53 20]\rm \begin{bmatrix} -5 & -3\ 2 & 0 \end{bmatrix}.

p(λ) = |λI - A|

⇒ p(λ) = λ+53 2λ\rm \begin{vmatrix} \lambda+5 & 3\ -2 & \lambda \end{vmatrix}

⇒ p(λ) = (λ )(λ +5) + (2)(3)

⇒ p(λ) = λ2 + 5λ + 6 

According to the Cayley - Hamilton theorem, p(A) = 0.

⇒ A2 + 5A + 6I = 0  --------(1)

⇒ A2 = - 5A - 6I ---------(2)

By multiplying equation (1) with A, we get

A3 + 5A2 + 6A = 0

⇒ A3 = -5 A2 -6A = -5 (- 5A - 6I ) -6A = 19 A + 30I

Additional Information

Matrix Multiplication:

  • Multiplication is only possible when the number of columns of the first matrix is equal to the number of rows of the second matrix.
  • A m×n matrix multiplied by a n×p matrix results in a m×p matrix.
  • Matrices are multiplied by multiplying each element of a row of the first m×n matrix with the corresponding elements of all the columns of the second n×p matrix to obtain the first row of the product matrix with p columns, and so on for all the m rows of the first matrix.
37

The maximum value of f(x) = x3 - 9x2 + 24x + 5 in the interval [1, 6] is

  1. ((a))

    21

  2. ((b))

    25

  3. ((c))

    41

  4. ((d))

    46

Show Answer
Answer: ((c))

41

f(x)=x39x2+24x+5;f\left( x \right) = {x^3} - 9{x^2} + 24x +5;

f(x)=3x218x+24{f^{'\left( x \right)}} = 3{x^2} - 18x + 24

f(x)=6x18{f^{''\left( x \right)}} = 6x - 18

To find maxima or minima

f(x)=0{f^{'\left( x \right)}} = 0

3x218x+24=03{x^2} - 18x + 24 = 0

x26x+8=0{x^2} - 6x + 8 = 0

x = 4 or x = 2

If x = 4

f'’(4) = 6

f'’(4) > 0

∴ minima may fall at 4 in the given domain

If x = 2

f'’(2) = -6

f'’(2) < 0

∴ maxima may fall at 2 in the given domain

Check the boundary condition along with x = 4 and x = 2

value of xf(x)
121
225
421
641

 

∴ The maximum value of given function is 41

38

If VA – VB = 6 V then VC – VD is

  1. ((a))

    -5 V

  2. ((b))

    2 V

  3. ((c))

    3 V

  4. ((d))

    6 V

Show Answer
Answer: ((a))

-5 V

VA – VB = 6 V

So current in the branch will be

IAB = 6/2 = 3 A

We can see, that the circuit is a one part circuit looking from terminal BD as shown below

For a one port network current entering one terminal, equals the current leaving the second terminal. Thus the outgoing current from A to B will be equal to the incoming current from D to C as shown.

i.e. IDC = IAB = 3 A

The total current in the resistor 1 Ω will be

I1 = 2 + IDC

= 2 + 3 = 5 A

VCD = 1 × (-I1)

= -5 V

39

The voltage gain AV of the circuit shown below is

  1. ((a))

    |AV| ≈ 200

  2. ((b))

    |AV| ≈ 100

  3. ((c))

    |AV| ≈ 20

  4. ((d))

    |AV| ≈ 10

Show Answer
Answer: ((d))

|AV| ≈ 10

The given circuit is a voltage – shunt or shunt – shunt negative feedback circuit.

RF = 100 kΩ

RS = 10 kΩ

Vo = - IS RF

=(VSRS)RF AV=VoVS=voltage gain=RtRS\begin{array}{l} = - \left( {\frac{{{V_S}}}{{{R_S}}}} \right){R_F}\ {A_V} = \frac{{{V_o}}}{{{V_S}}} = voltage\ gain = \frac{{ - {R_t}}}{{{R_S}}} \end{array}

AV = -10

|AV| ≈ 10.

40

The state transition diagram for the logic circuit shown is

  1. ((a))

  2. ((b))

  3. ((c))

  4. ((d))

Show Answer
Answer: ((d))

Concept:

Output expression (Y) for 2 × 1 MUX is given as

Y = A̅ x0 + A x1          ---(1)

The next state (Qn + 1) of D flip flop is:

Qn + 1 = D           ---(2)

Analysis:

From given circuit:

D = Y, x1 = Q, x0 = Q̅

We know that

Y = A̅ x0 + A x1

From given data,

D = A̅ Q̅ + AQ

From eqn (2) θn+1 = A̅ Q̅ + A Q

APresent state (Q)Next state (Qn+1)
00Q = 1
01Q = 0
10Q = 0
11Q = 1

   

So, the state transition diagram will be:

41

Let y[n] denote the convolution of h[n] and g[n], where h[n] = (1/2)n u[n] and g[n] is a causal sequence. If y[0] = 1 and y[1] = ½, then g[1] equals

  1. ((a))

    0

  2. ((b))

    ½

  3. ((c))

    1

  4. ((d))

    3/2

Show Answer
Answer: ((a))

0

Convolution sum is defined as

\(y\left[ n \right] = h\left[ n \right]*g\left[ n \right] = \mathop \sum \limits_{k = - \infty }^\infty h\left[ k \right]g\left[ {n - k} \right]\)

For causal sequence,

y[n] = h[0] g[n] + h[1] g [n-1] + h[2] g[n-2] +….

For n = 0,

y[0] = h[0] g[0] + h[1] g[-1] +…..

= h [0] g[0]            (g[-1] = g[-2] =……..0)

y[0] = h[0] g[0]

For. n =1,  y [1] = h [0] g [1] + h [1] g [0] + h [2] g [-1] + ……

y [1] = h [0] g [1] + h [1] g [0] +....

12=g[1]+12g[0]\frac{1}{2} = g\left[ 1 \right] + \frac{1}{{2}}g\left[ 0 \right]

Now, g[0]=y[0]h[0]=11=1g\left[ 0 \right] = \frac{{y\left[ 0 \right]}}{{h\left[ 0 \right]}} = \frac{1}{1} = 1

g [1] = 0.5 - 0.5 = 0.

42

The circuit shown is a

  1. ((a))

    low pass filter with f3dB=1(R1+R2)C:rad/sf_{3dB}=\frac{1}{(R_1+R_2)C}:rad/s

  2. ((b))

    high pass filter with f3dB=1R1C:rad/sf_{3dB}=\frac{1}{R_1C}:rad/s

  3. ((c))

    low pass filter with f3dB=1R1C:rad/sf_{3dB}=\frac{1}{R_1C}:rad/s

  4. ((d))

    high pass filter with f3dB=1(R1+R2)C:rad/sf_{3dB}=\frac{1}{(R_1+R_2)C}:rad/s

Show Answer
Answer: ((b))

high pass filter with f3dB=1R1C:rad/sf_{3dB}=\frac{1}{R_1C}:rad/s

Active high pass filter:

The simplest HPF using an operational amplifier can be achieved by placing a capacitor in series with one of the resistors in the inverting amplifier circuit as shown.

Apply KCL at the inverting terminal node, we get

Vi0R1+1jωC=0V0R2\frac{{{V_i} - 0}}{{{R_1} + \frac{1}{{jω C}}}} = \frac{{0 - {V_0}}}{{{R_2}}}

V0Vi=R2R1+1jωC ⇒ \frac{{{V_0}}}{{{V_i}}} = \frac{{ - {R_2}}}{{{R_1} + \frac{1}{{jω C}}}}

Case 1:

If the frequency ω = 0 rad/sec

 V0Vi=R2R1+10=R2R1+=0 \Rightarrow \frac{{{V_0}}}{{{V_i}}} = \frac{{ - {R_2}}}{{{R_1} + \frac{1}{0}}} = \frac{{ - {R_2}}}{{{R_1} + ∞ }} = 0

So, for the frequency ω = 0, the output V0 =0

Case 2:

If the frequency ω = ∞ rad/sec

V0Vi=R2R1+1=R2R1+0=R2R1 \Rightarrow \frac{{{V_0}}}{{{V_i}}} = \frac{{ - {R_2}}}{{{R_1} + \frac{1}{∞ }}} = \frac{{ - {R_2}}}{{{R_1} + 0}} = \frac{{ - {R_2}}}{{{R_1}}}

So, for frequency ω = ∞ , the output V0=R2R1Vi{V_0} = \frac{{ - {R_2}}}{{{R_1}}}{V_i}

By, observing case 1 and case 2 we can say that the above circuit is allowing high frequencies but the lower frequencies are not allowed. Hence the above circuit is a high pass filter (HPF)

And the cutoff frequency or the breakpoint of the filter can be calculated very easily by working out of the frequency at which the reactance of the capacitor equals the resistance resistor to which the capacitor is connected in series.

So, Xc = R1

1ωc;C=R1 \Rightarrow \frac{1}{{{ω _c};C}} = {R_1}

ωc=1R1C \Rightarrow {ω _c} = \frac{1}{{{R_1}C}}

Where ωc is the cutoff frequency in rad/sec.

Hence the given circuit is a High pass filter with a cutoff frequency 1R1C\frac{1}{{{R_1}C}}.

43

For the system below, SD1 and SD2 are complex power demands at bus 1 and bus 2 respectively. If |V2| = 1 pu, the VAR rating of the capacitor (  QG2) connected at bus 2 is

  1. ((a))

    0.2 pu

  2. ((b))

    0.268 pu

  3. ((c))

    0.312 pu

  4. ((d))

    0.4 pu

Show Answer
Answer: ((b))

0.268 pu

Real power Pr=VsVrxsinδ{P_r} = \frac{{\left| {{V_s}} \right|\left| {{V_r}} \right|}}{{\left| x \right|}}\sin \delta 

1=1.0×1.00.5sinδδ=30\Rightarrow 1 = \frac{{1.0 \times 1.0}}{{0.5}}\sin \delta \Rightarrow \delta = 30^\circ

Reactive power ϕr=VSVrxcosδV2x{\phi _r} = \frac{{\left| {{V_S}} \right|\left| {{V_r}} \right|}}{{\left| x \right|}}\cos \delta - \frac{{{V^2}}}{{\left| x \right|}}

=(1.0)(1.0)0.5cos30(1.0)20.5 = \frac{{\left( {1.0} \right)\left( {1.0} \right)}}{{0.5}}\cos 30 - \frac{{{{\left( {1.0} \right)}^2}}}{{0.5}}

= -0.268

QC + Qr = 0 ⇒ Qr = 0.268

44

A cylinder rotor generator delivers 0.5 pu power in the steady – state to an infinite bus through a transmission line of reactance 0.5 pu. The generator no-load voltage is 1.5 pu and the infinite bus voltage is 1 pu. The inertia constant of the generator is 5 MW – s / MVA and the generator reactance in 1 pu. The critical clearing angle, in degrees, for a three – phase dead short circuit fault at the generator terminal is

  1. ((a))

    53.5

  2. ((b))

    60.2

  3. ((c))

    70.8

  4. ((d))

    79.6

Show Answer
Answer: ((d))

79.6

PS = Pe1 = 0.5

Before fault Pm1=EVX=1.5×1.01.5=1.0{P_{m1}} = \frac{{{E_V}}}{X} = \frac{{1.5 \times 1.0}}{{1.5}} = 1.0 

During fault Pm2 = 0,

After the fault Pm3 = 1.0

\(\begin{array}{l} \delta = {\sin ^{ - 1}}\left( {\frac{{{P_S}}}{{{P_{m1}}}}} \right) = {\sin ^{ - 1}}\left( {\frac{{0.5}}{{1.0}}} \right) = 30^\circ \ {\delta _o} = \frac{{30 \times \pi }}{{180}} = 0.52\ rad\ {\delta {max}} = 180 - {\sin ^{ - 1}}\left( {\frac{{{P_S}}}{{{P{m3}}}}} \right)\ = 180 - {\sin ^{ - 1}}\left( {\frac{{0.5}}{1}} \right) = 150^\circ \ {\delta _{\max \left( {radians} \right)}} = \frac{{150 \times \pi }}{{180}} = 2.618rad\ {\delta _C} = {\cos ^{ - 1}}\left[ {\frac{{{P_S}\left( {{\delta _{max}} - {\delta o}} \right) + {P{m3}}\cos {\delta {max}}}}{{{P{m3}}}}} \right]\ = {\rm{ }}79.45^\circ \end{array}\)

45

In the circuit shown, an ideal switch S is operated at 100 KHz with a duty ratio of 50%. Given that Δ icis 1.6 A peak to peak and Iois 5 A dc, the peak current in S is

  1. ((a))

    6.6 A

  2. ((b))

    5.0 A

  3. ((c))

    5.8 A

  4. ((d))

    4.2 A

Show Answer
Answer: ((c))

5.8 A

Solution:-

Input voltage, Vin = 24V

Operating frequency, f = 100 kHz

Duty ratio, D = 50%

Inductor peak-to-peak current ripple, ΔIL = 1.6 A

Average inductor current, ILavg = 5 A

<br>

The peak inductor current ILpeak is calculated as:

ILpeak = ILavg + (ΔIL / 2) = 5 A + (1.6 A / 2) = 5 A + 0.8 A = 5.8 A

Since the peak current in the switch S is the same as the peak inductor current during the on-state, the peak current in S is:

ISpeak = 5.8 A

46

A 220V 15KW 1000rpm shunt motor with armature resistance of 0.25  has a rated line current of 68 A and a rated field current of 2.2A. The change in field flux required to obtain a speed of 1600 rpm while drawing a line current of 52.8 A and a field current of 1.8A is

  1. ((a))

    18.18% increase

  2. ((b))

    18.18% decrease

  3. ((c))

    36.36% increase

  4. ((d))

    36.36% decrease

Show Answer
Answer: ((d))

36.36% decrease

E1=22065.8×0.25=203.55 V E2=22051×0.25=207.25 V N2N1=E2E1×ϕ1ϕ2 16001000=207.25203.55×ϕ1ϕ2 ϕ1ϕ2=1.571 ϕ1ϕ2ϕ1=0.3636\begin{array}{l} {E_1} = 220 - 65.8 \times 0.25 = 203.55\ V\ {E_2} = 220 - 51 \times 0.25 = 207.25\ V\ \frac{{{N_2}}}{{{N_1}}} = \frac{{{E_2}}}{{{E_1}}} \times \frac{{{\phi _1}}}{{{\phi _2}}}\ \frac{{1600}}{{1000}} = \frac{{207.25}}{{203.55}} \times \frac{{{\phi _1}}}{{{\phi _2}}}\ \frac{{{\phi _1}}}{{{\phi _2}}} = 1.571\ \frac{{{\phi _1} - {\phi _2}}}{{{\phi _1}}} = 0.3636 \end{array}

Hence there is a 36.36% decrease

47

A fair coin is tossed till a head appears for the first time. The probability that the number of required tosses is odd, is

  1. ((a))

    1/3

  2. ((b))

    1/2

  3. ((c))

    2/3

  4. ((d))

    3/4

Show Answer
Answer: ((c))

2/3

Concept:

For a geometric progression given as:

a, ar2, ar3, …, ∞

Where,

a > 0 and 0 < r < 1

The sum is given by:

Sum=a1rSum=\frac{a}{1-r}

Calculation:

The probability of appearing a head is 1/2. If the number of required tosses is odd, we have the following sequence of events.

H, TTH, TTTTH, …..

The required Probability P will be:

P=12+(12)3+(12)5+P = \frac{1}{2} + {\left( {\frac{1}{2}} \right)^3} + {\left( {\frac{1}{2}} \right)^5} + \ldots

=12114=23 = \frac{{\frac{1}{2}}}{{1 - \frac{1}{4}}} = \frac{2}{3}

48

The direction of vector A is radially outward from the origin, with n |A| = krn where r2 = x2 + y2 + z2 and k is a constant. The value of n for which ∇⋅A = 0 is

  1. ((a))

    -2

  2. ((b))

    2

  3. ((c))

    1

  4. ((d))

    0

Show Answer
Answer: ((a))

-2

A=k.rn,r2=x2+y2+z2\left| {\vec A} \right| = k.{r^n},{r^2} = {x^2} + {y^2} + {z^2}

A=krn.a^r \Rightarrow \vec A = k{r^n}.{\hat a_r} ........ (Given radial outward) 

In spherical coordinates

.A=1r2r(r2Ar)+0+0=1r2;r(r2.krn)\vec \nabla .{\rm{\vec A}} = \frac{1}{{{{\rm{r}}^2}}}\frac{\partial }{{\partial {\rm{r}}}}\left( {{{\rm{r}}^2}{{\rm{A}}_{\rm{r}}}} \right) + 0 + 0 = \frac{1}{{{{\rm{r}}^2}}}{\rm{;}}\frac{\partial }{{\partial {\rm{r}}}}\left( {{{\rm{r}}^2}.{\rm{k}}{{\rm{r}}^{\rm{n}}}} \right)

.A=kr2r(r(n+2))=kr2(n+2)(r(n+1))\vec \nabla .{\rm{\vec A}} = \frac{{\rm{k}}}{{{{\rm{r}}^2}}}\frac{\partial }{{\partial {\rm{r}}}}\left( {{r^{\left( {n + 2} \right)}}} \right)=\frac{{\rm{k}}}{{{{\rm{r}}^2}}}(n+2){{}}\left( {{r^{\left( {n + 1} \right)}}} \right)

⇒ For  .A=0, n+2=0\vec \nabla .{\rm{\vec A}} = 0,~n+2 =0

n=2n = - 2

49

Consider the differential equation

\(\frac{{{d^2}y\left( t \right)}}{{d{t^2}}} + 2\frac{{dy\left( t \right)}}{{dt}} + y\left( t \right) = \delta \left( t \right)\ with\ y\left( t \right){|{t = {0^ - }}} = - 2\ and\ \frac{{dy}}{{dt}}{|{t = {0^ - }}} = 0\)

The numerical value of dydtt=0+\frac{{dy}}{{dt}}{|_{t = {0^ + }}} is

  1. ((a))

    -2

  2. ((b))

    -1

  3. ((c))

    0

  4. ((d))

    1

Show Answer
Answer: ((d))

1

d2ydt2+2dydt+y=δ(t)\frac{{{d^2}y}}{{d{t^2}}} + \frac{{2dy}}{{dt}} + y = \delta \left( t \right)

Taking Laplace transform with initial conditions,

[s2y(s)sy(0)dydtt=0]+2[sy(s)y(0)]+y(s)=1 (s2y(s)+2s0)+2[sy(s)+2]+y(s)=1 y(s)(s2+2s+1)=12s4 y(s)=2s3s2+2s+1\begin{array}{l} \left[ {{s^2}y\left( s \right) - sy\left( 0 \right) - \frac{{dy}}{{dt}}{|_{t = 0}}} \right] + 2\left[ {sy\left( s \right) - y\left( 0 \right)} \right] + y\left( s \right) = 1\ \Rightarrow \left( {{s^2}y\left( s \right) + 2s - 0} \right) + 2\left[ {sy\left( s \right) + 2} \right] + y\left( s \right) = 1\ y\left( s \right)\left( {{s^2} + 2s + 1} \right) = 1 - 2s - 4\ y\left( s \right) = \frac{{ - 2s - 3}}{{{s^2} + 2s + 1}} \end{array}

We know that, If y(t)Zy(s)y\left( t \right)\mathop \leftrightarrow \limits^Z y\left( s \right)

Then, dydtZsy(s)y(0)\frac{{dy}}{{dt}}\mathop \leftrightarrow \limits^Z sy\left( s \right) - y\left( 0 \right)

So, sy(s)y(0)=s+2(s+1)2=1s+1+1(s+1)2sy\left( s \right) - y\left( 0 \right) = \frac{{s + 2}}{{{{\left( {s + 1} \right)}^2}}} = \frac{1}{{s + 1}} + \frac{1}{{{{\left( {s + 1} \right)}^2}}}

Taking inverse Laplace,

dydt=etu(t)+tetu(t)\frac{{dy}}{{dt}} = {e^{ - t}}u\left( t \right) + t{e^{ - t}}u\left( t \right)

At t=0+,dydtt=0+=e0+0=1t = {0^ + },\frac{{dy}}{{dt}}{|_{t = {0^ + }}} = {e^0} + 0 = 1

50

Assuming both the voltage sources are in phase, the value of R for which maximum power is transferred from circuit A to circuit B is

  1. ((a))

    0.8 Ω

  2. ((b))

    1.4 Ω

  3. ((c))

    2 Ω

  4. ((d))

    2.8 Ω

Show Answer
Answer: ((a))

0.8 Ω

We obtain Thevenin equivalent of circuit B

Thevenin impedance:

Thevenin Voltage: Vth = 3∠0° V

Now, circuit becomes as

Current in the circuit,

I1 = (10-3)/(2 + R)

Power transfer from circuit A to B

P = (I1)2R + 3 I1

= (42 + 70 R)/(2 + R)2

dP/dR = 0

⇒ (2 + R) [(2 + R) 70 – (42 + 70 R) 2] = 0

⇒ R = 0.8 Ω

51

State variable description of an LTI system is given by

\(\left[ {\begin{array}{{20}{c}} {{{\dot x}_1}}\ {{{\dot x}_2}}\ {{{\dot x}_3}} \end{array}} \right] = \left[ {\begin{array}{{20}{c}} 0&{{a_1}}&0\ 0&0&{{a_2}}\ {{a_3}}&0&0 \end{array}} \right]\left[ {\begin{array}{{20}{c}} {{x_1}}\ {{x_3}}\ {{x_3}} \end{array}} \right] + \left[ {\begin{array}{{20}{c}} 0\ 0\ 1 \end{array}} \right]U\)

\(Y = \left[ {\begin{array}{{20}{c}} 1&0&0 \end{array}} \right]\left[ {\begin{array}{{20}{c}} {{x_1}}\ {{x_2}}\ {{x_3}} \end{array}} \right]\)

Where Y is the output and u is input. System is controllable for

  1. ((a))

    a1 ≠ 0, a2 = 0, a3 ≠ 0

  2. ((b))

    a1 = 0, a2 ≠ 0, a3 = 0

  3. ((c))

    a1 = 0, a2 ≠ 0, a3 ≠ 0

  4. ((d))

    a1 ≠ 0, a2 ≠ 0, a3 = 0

Show Answer
Answer: ((d))

a1 ≠ 0, a2 ≠ 0, a3 = 0

\({Q_c} = \left[ {\begin{array}{*{20}{c}} B&{AB}&{{A^2}B} \end{array}} \right]\)

\({Q_c} = \left[ {\begin{array}{*{20}{c}} 0&0&{{a_1}{a_2}}\ 0&{{a_2}}&0\ 1&0&0 \end{array}} \right]\)

System is controllable if |QC| ≠ 0

a1a2 (0 – a2) ≠ 0

a1a220- {a_1} \cdot a_2^2 \ne 0

Hence condition for controllability is

a1 ≠ 0, a2 ≠ 0, a3 = 0

52

The Fourier transform of a signal h(t) is H (jω) = (2 cosω ) (sin2ω) / ω . The value of h(0) is

  1. ((a))

    ¼

  2. ((b))

    ½

  3. ((c))

    1

  4. ((d))

    2

Show Answer
Answer: ((c))

1

H(jω)=(2cosω)(sin2ω)ω =sin3ωω+sinωω\begin{array}{l} H\left( {j\omega } \right) = \frac{{\left( {2\cos \omega } \right)\left( {\sin 2\omega } \right)}}{\omega }\ = \frac{{\sin 3\omega }}{\omega } + \frac{{sin\omega }}{\omega } \end{array}

We know that the inverse Fourier transform of sinc function is a rectangular function.

A rect(tτ)Aτ Sa(ωτ2)A~rect(\frac{t}{\tau}) \leftrightarrow A \tau ~Sa(\frac{\omega \tau}{2})

Now,

Sa(ωτ2)=sin (ωτ2)ωτ2Sa(\frac{\omega \tau}{2}) = \frac{sin~(\frac{\omega \tau}{2})}{\frac{\omega \tau}{2}}

\(\frac{sin 3\omega}{\omega} = 3 \frac{sin(3\omega)}{3\omega}\)

By comparing, we get

τ/2=3,Aτ=3\tau/2 = 3, A\tau = 3

hence, A = 0.5

2) 

\(\frac{sin \omega}{\omega} = 1\times \frac{sin(\omega \times 1)}{\omega \times 1}\)

By comparing, we get

τ/2=1,Aτ=1\tau/2 = 1, A\tau = 1

hence, A = 0.5

 

So, inverse Fourier transform of H (jω)

h(t) = h(t) + h2(t)

h(0) = h1(0) + h2­­(0)

12+12=1\frac{1}{2}+\frac{1}{2} = 1

53

The feedback system shown below oscillates at 2 rads/sec. when

  1. ((a))

    k = 2 and a = 0.75

  2. ((b))

    k = 4 and a = 0.5

  3. ((c))

    k = 3 and a = 0.75

  4. ((d))

    k = 2 and a = 0.5

Show Answer
Answer: ((a))

k = 2 and a = 0.75

Characteristic equation is       s3 + as2 + (k + 2) s + (k + 1) = 0

Routh array

s31k + 2
s2ak + 1
s1a(k+2)(k+1)a\frac{{a\left( {k + 2} \right) - \left( {k + 1} \right)}}{a}
s0k + 1
<br>

System oscillates if a(k+2)(k+1)a=0\frac{{a\left( {k + 2} \right) - \left( {k + 1} \right)}}{a} = 0

ak + 2a = k + 1

a=k+1k+2a = \frac{{k + 1}}{{k + 2}}

System oscillates at ω = 2 rad/sec

as2 + k + 1 = 0

k+1k+2s2+k+1=0\frac{{k + 1}}{{k + 2}}{s^2} + k + 1 = 0

s2 = – (k + 2)

s=±k+2;js = \pm \sqrt {k + 2} ;j

Comparing k+2=2\sqrt {k + 2} = 2

k = 2

a=k+1k+2=2+12+2=0.75a = \frac{{k + 1}}{{k + 2}} = \frac{{2 + 1}}{{2 + 2}} = 0.75

54

The input x(t) and output y(t) of a system are related as y(t)=tx(τ)cos(3τ)dτ.y(t)=\int_{-\infty}^t x(\tau)cos(3\tau)d\tau. The system is

  1. ((a))

    time-invariant and stable

  2. ((b))

    stable and not time-invariant

  3. ((c))

    time-invariant and not stable

  4. ((d))

    not time-invariant and not stable

Show Answer
Answer: ((d))

not time-invariant and not stable

  1. Time Invariant and Time Variant System:

If in a system, a delay in the input leads to same delay in the output, then such system is known as time invariant system. Otherwise It will be time variant system.

  1. Stable and Unstable system:

The system is sold to be stable only when the bounded output for the input.

For a bounded input if output is unbounded then system is said to be UNSTABLE.

Condition:

\(\mathop \smallint \nolimits_{ - \infty }^\infty \left| {h\left( t \right)} \right|dt < \infty \) or finite.

Where h(t) is impulse response of system.

Solution:

Given, \(y\left( t \right) = \mathop \smallint \nolimits_{ - \infty }^t x\left( \tau \right)\cos \left( {3\tau} \right)d\tau\) 

Check for time-invariance:

Since y’(t) ≠ y (t – t0) so it is time-variant

Stability:

Suppose input x(t) = cos 3t

\(y\left( t \right) = \mathop \smallint \nolimits_{ - \infty }^t {\cos ^2}3\tau dt = \mathop \smallint \nolimits_{ - \infty }^t \left( {\frac{{1 + \cos 6\tau }}{2}} \right)d\tau ;\)

\(y\left( t \right) = [\left. {\frac{1}{2}t\tau } \right|{ - \infty }^t + \frac{1}{2}\sin \left. {\frac{{6\tau }}{6}} \right|{ - \infty }^t\)

Since y(t) → ∞, it is unbounded of P so this is an unstable system.

TRICK:

→ check for stability: try to find at least one input value for which output will be unbounded.

e.g. y(t)=ex(t5)t5y\left( t \right) = \frac{{{e^x}\left( {t - 5} \right)}}{{t - 5}} at t = 5 y(t) → ∞ - unbounded.

→ check for variance: If any coefficient if input is function of time (t) then it will be time variant.

e.g. tx(t), etx(t), sin t x(t)

55

An analog voltmeter uses external multiplier setting with a multiplier setting of 20 kΩ, it reads 440 V and with a multiplier setting of 80 kΩ it reads 352 V. For a multiplier setting of 40 kΩ the voltmeter reads______.

  1. ((a))

    371 V

  2. ((b))

    383 V

  3. ((c))

    394 V

  4. ((d))

    406 V

Show Answer
Answer: ((d))

406 V

Multiplier setting = 20 kΩ

Meter resistance = x

Total resistance = 20 kΩ + x = R1

Voltmeter reading (V1) = 440 V

V1αI1x I1α1R1\begin{array}{l} {V_1}\alpha {I_1}x\ {I_1}\alpha \frac{1}{{{R_1}}} \end{array}

For multiplier setting = 80 kΩ

Meter resistance = x

Total resistance = 80 KΩ + x = R2

Voltmeter reading (V2) = 352 V

V2αI2x I2α1R2 V2V1=I2I1=R1R2 352440=20+x80+xx=220 kΩ\begin{array}{l} {V_2}\alpha {I_2}x\ {I_2}\alpha \frac{1}{{{R_2}}}\ \frac{{{V_2}}}{{{V_1}}} = \frac{{{I_2}}}{{{I_1}}} = \frac{{{R_1}}}{{{R_2}}}\ \frac{{352}}{{440}} = \frac{{20 + x}}{{80 + x}} \Rightarrow x = 220\ k{\rm{\Omega }} \end{array}

For multiplier setting = 40 KΩ

R3 = 260 kΩ

V3V1=I3I1=R1R3V3440=240260V3=406 V\frac{{{V_3}}}{{{V_1}}} = \frac{{{I_3}}}{{{I_1}}} = \frac{{{R_1}}}{{{R_3}}} \Rightarrow \frac{{{V_3}}}{{440}} = \frac{{240}}{{260}} \Rightarrow {V_3} = 406\ V

56

The locked rotor in a 3 phase star connected 15 kW 4 pole 230 V 50 Hz IM runs at rated conditions of 50A. Neglecting losses and magnetising current the approximate locked rotor line current drawn when the motor is connected to 236 V 57 Hz is

  1. ((a))

    58.5A

  2. ((b))

    45.0A

  3. ((c))

    45.7A

  4. ((d))

    55.6A

Show Answer
Answer: ((b))

45.0A

Ise=VXse α vf Ise nw=50×236230×5057 =45A\begin{array}{l} {I_{se}} = \frac{V}{{{X_{se}}}}\ \alpha\ \frac{v}{f}\ \therefore {I_{se}}\ nw = 50 \times \frac{{236}}{{230}} \times \frac{{50}}{{57}}\ = 45A \end{array}

57

A  single phase 10KVA 50Hz transformer 1 KV primary winding with current 0.5A and 55W  at the rated voltage and frequency, on no load. A second transformer has a core with all its linear dimensions √2 times the corresponding dimensions of the first transformer. The core thickness and laminations are the same in both the transformers. The primary winding of both the transformers have same number of turns. If the rated voltage of 2KV at 50Hz is applied to the primary of the second transformer, the no load current and power are:

  1. ((a))

    0.7A,77.8 W

  2. ((b))

    0.7A,155.6 W

  3. ((c))

    1 A,110 W

  4. ((d))

    1 A,220 W

Show Answer
Answer: ((b))

0.7A,155.6 W

Core loss α core volume

∴ New loss (2)3×55=155.6W{\left( {\sqrt 2 } \right)^3} \times 55 = 155.6W

Core loss Pi=VIc{P_i} = V{I_c}

Ic1=551000=0.055 A Ic2=(2)3Ic1\begin{array}{l} {I_{{c_1}}} = \frac{{55}}{{1000}} = 0.055\ A\ {I_{{c_2}}} = {\left( {\sqrt 2 } \right)^3}{I_{{c_1}}} \end{array}

From the data for 2nd transformer

Ic2=0.155 A Im1=0.496[(0.5)2(0.055)2=0.496]\begin{array}{l} {I_{{c_2}}} = 0.155\ A\ \therefore {I_{{m_1}}} = 0.496\left[ {\therefore \sqrt {{{\left( {0.5} \right)}^2} - {{\left( {0.055} \right)}^2}} = 0.496} \right] \end{array}

Reluctance R2=R12{R_2} = \frac{{{R_1}}}{{\sqrt 2 }}

m1=40004.44N1f{\emptyset _{{m_1}}} = \frac{{4000}}{{4.44{N_1}f}}             m2=20004.44 N1f{\emptyset _{{m_2}}} = \frac{{2000}}{{4.44\ {N_1}f}}

\(\begin{array}{l} {\emptyset _{{m_2}}} = 2{\emptyset _{{m_1}}}\ {\emptyset _{{m_1}}} = \frac{{{N_1}{I_m}_2}}{{{R_1}}}\ {\emptyset {{m_2}}} = \frac{{{N_1}{I_m}2}}{{\frac{{{R_1}}}{{\surd 2}}}}\ \therefore {I{{m_2}}} = \surd 2{I{{m_1}}}\ = \sqrt 2 \times 0.496 \end{array}\)

= 0.702 A

I0=Im12+Ic22 =(0.7025)2(0.155)2=0.718 A\begin{array}{l} \therefore {I_0} = \sqrt {I_{{m_1}}^2 + I_{{c_2}}^2} \ = \sqrt {{{\left( {0.7025} \right)}^2} - {{\left( {0.155} \right)}^2}} = 0.718\ A \end{array}

In the 3-phase inverter circuit shown, the load is balanced and the gating scheme is 180°-conduction mode. All the switching devices are ideal. (Vd = 300 V)

58

The rms value of load phase voltage is

  1. ((a))

    106.1 V

  2. ((b))

    141.4 V

  3. ((c))

    212.2 V

  4. ((d))

    282.8 V

Show Answer
Answer: ((b))

141.4 V

Concept:

Parameter180° conduction mode120° conduction mode
Phase voltage (Vph)23Vs\frac{{\sqrt 2 }}{3}{V_s}Vs6\frac{{{V_s}}}{{\sqrt 6 }}
Line voltage (VL)23Vs\sqrt {\frac{2}{3}} {V_s}Vs2\frac{{{V_s}}}{{\sqrt 2 }}
RMS load current (Ior)23RVs\frac{{\sqrt 2 }}{{3R}}{V_s}Vs6R\frac{{{V_s}}}{{\sqrt 6 R}}
RMS thyristor current (ITr)Vs3R\frac{{{V_s}}}{{3R}}Vs23R\frac{{{V_s}}}{{2\sqrt 3 R}}

 

Calculation:

A three-phase voltage source inverter supplying equivalent star load.

Equivalent star load resistance is,

Rph=20;Ω Vph=23Vdc=23×300=2002V=141.42;V{R_{ph}} =20;{\rm{\Omega }}\ {V_{ph}} = \frac{{\sqrt 2 }}{3}{V_{dc}} = \frac{{\sqrt 2 }}{3} \times 300 = 200\sqrt 2 V = 141.42;V

59

If the dc bus voltage Vd = 300 V, the power consumed by 3-phase load is

  1. ((a))

    1.5 kW

  2. ((b))

    2.0 kW

  3. ((c))

    2.5 kW

  4. ((d))

    3.0 kW

Show Answer
Answer: ((d))

3.0 kW

Concept:

Parameter180° conduction mode120° conduction mode
Phase voltage (Vph)23Vs\frac{{\sqrt 2 }}{3}{V_s}Vs6\frac{{{V_s}}}{{\sqrt 6 }}
Line voltage (VL)23Vs\sqrt {\frac{2}{3}} {V_s}Vs2\frac{{{V_s}}}{{\sqrt 2 }}
RMS load current (Ior)23RVs\frac{{\sqrt 2 }}{{3R}}{V_s}Vs6R\frac{{{V_s}}}{{\sqrt 6 R}}
RMS thyristor current (ITr)Vs3R\frac{{{V_s}}}{{3R}}Vs23R\frac{{{V_s}}}{{2\sqrt 3 R}}

 

Calculation:

A three-phase voltage source inverter supplying equivalent star load.

Equivalent star load resistance is,

Rph=20;Ω Vph=23Vdc=23×300=2002V=141.42;V P=3Vph2R=3×(141.42)220=3kW\begin{array}{l} {R_{ph}} =20;{\rm{\Omega }}\ {V_{ph}} = \frac{{\sqrt 2 }}{3}{V_{dc}} = \frac{{\sqrt 2 }}{3} \times 300 = 200\sqrt 2 V = 141.42;V\ P = 3\frac{{{V_p}{h^2}}}{R} = 3 \times \frac{{{{\left( {141.42 } \right)}^2}}}{{20}} = 3kW \end{array}

With 10 V dc connected at port A in the linear nonreciprocal two-port network shown below, the following were observed:

i)  1 Ω connected at port B draws a current of 3 A

ii)  2.5 Ω connected at port B draws a current of 2 A

60

With 6 V dc connected at port A, 1 Ω connected at port B draws 7/3 A. If 8 V dc is connected to port A, the open circuit voltage at port B is

  1. ((a))

    6 V

  2. ((b))

    7 V

  3. ((c))

    8 V

  4. ((d))

    9 V

Show Answer
Answer: ((c))

8 V

Now, when 6 V connected at port A let thevenin voltage seen at port B is Vth,6 V . Here RL = 1 Ω and IL = 7/3 A

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%MathType!Translator!2!1!LaTeX.tdl!LaTeX2.09andlater!%MathType!MTEF!2!1!+%feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn%hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr%4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9LqJc9%vqaqpepm0xbba9pwe9Q8fs0yqaqpepae9pg0FirpepeKkFr0xfrx%frxb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8%qacqGH9aqpcaaIYaGaey41aq7aaSaaa8aabaWdbiaaiEdaa8aabaWd%biaaiodaaaGaey4kaSYaaSaaa8aabaWdbiaaiEdaa8aabaWdbiaaio%daaaGaeyypa0JaaG4naiaadAfaaaa!410C!=2×73+73=7V%MathType!End!2!1!\% MathType!Translator!2!1!LaTeX.tdl!LaTeX 2.09 and later! \% MathType!MTEF!2!1!+- \% feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn \% hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr \% 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq-Jc9 \% vqaqpepm0xbba9pwe9Q8fs0-yqaqpepae9pg0FirpepeKkFr0xfr-x \% fr-xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8 \% qacqGH9aqpcaaIYaGaey41aq7aaSaaa8aabaWdbiaaiEdaa8aabaWd \% biaaiodaaaGaey4kaSYaaSaaa8aabaWdbiaaiEdaa8aabaWdbiaaio \% daaaGaeyypa0JaaG4naiaadAfaaaa!410C! = 2 \times \frac{7}{3} + \frac{7}{3} = 7V\% MathType!End!2!1!

This is a linear network, so Vth­ at port B can be written as

Vth = V1 α + β

Where V1 is the input applied at port A.

We have V1 = 10 V, Vth,10 V = 9 V

9 = 10 α + β

when V1 = 6 V, Vth,6 V = 9 V

7 = 6 α + β

⇒ α = 0.5, β = 4

Thus, with any voltage V1 applied at port A, thevenin voltage or open circuit voltage at port B will be

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V1 = 8 V

Vth,8 V = (0.5 × 8) + 4 = 8 = open circuit voltage

61

With 10 V dc connected at port A, the current drawn by 7 Ω connected at port B is

  1. ((a))

    3/7 A

  2. ((b))

    5/7 A

  3. ((c))

    1 A

  4. ((d))

    9/7 A

Show Answer
Answer: ((c))

1 A

When 10 V is connected at port A the network is

Now, we obtain Thevenin equivalent for the circuit seen at load terminal, let thevenin voltage is Vth ,10 V with 10 V applied at port A and thevenin resistance is Rth.

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For RL = 1 Ω, IL = 3 A

%MathType!Translator!2!1!LaTeX.tdl!LaTeX2.09andlater!%MathType!MTEF!2!1!+%feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn%hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr%4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9LqJc9%vqaqpepm0xbba9pwe9Q8fs0yqaqpepae9pg0FirpepeKkFr0xfrx%frxb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8%qacaaIZaGaeyypa0ZaaSaaa8aabaWdbiaadAfapaWaaSbaaSqaa8qa%caWG0bGaamiAaiaacYcacaaIXaGaaGimaiaadAfaa8aabeaaaOqaa8%qacaWGsbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGH%RaWkcaaIXaaaaaaa!430C!3=Vth,10VRth+1%MathType!End!2!1!\% MathType!Translator!2!1!LaTeX.tdl!LaTeX 2.09 and later! \% MathType!MTEF!2!1!+- \% feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn \% hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr \% 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq-Jc9 \% vqaqpepm0xbba9pwe9Q8fs0-yqaqpepae9pg0FirpepeKkFr0xfr-x \% fr-xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8 \% qacaaIZaGaeyypa0ZaaSaaa8aabaWdbiaadAfapaWaaSbaaSqaa8qa \% caWG0bGaamiAaiaacYcacaaIXaGaaGimaiaadAfaa8aabeaaaOqaa8 \% qacaWGsbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGH \% RaWkcaaIXaaaaaaa!430C! 3 = \frac{{{V_{th,10V}}}}{{{R_{th}} + 1}}\% MathType!End!2!1!

For RL = 2.5 Ω, IL = 2 A

%MathType!Translator!2!1!LaTeX.tdl!LaTeX2.09andlater!%MathType!MTEF!2!1!+%feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn%hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr%4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9LqJc9%vqaqpepm0xbba9pwe9Q8fs0yqaqpepae9pg0FirpepeKkFr0xfrx%frxb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8%qacaaIYaGaeyypa0ZaaSaaa8aabaWdbiaadAfapaWaaSbaaSqaa8qa%caWG0bGaamiAaiaacYcacaaIXaGaaGimaiaadAfaa8aabeaaaOqaa8%qacaWGsbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGH%RaWkcaaIYaGaaiOlaiaaiwdaaaaaaa!447D!2=Vth,10VRth+2.5%MathType!End!2!1!\% MathType!Translator!2!1!LaTeX.tdl!LaTeX 2.09 and later! \% MathType!MTEF!2!1!+- \% feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn \% hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr \% 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq-Jc9 \% vqaqpepm0xbba9pwe9Q8fs0-yqaqpepae9pg0FirpepeKkFr0xfr-x \% fr-xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8 \% qacaaIYaGaeyypa0ZaaSaaa8aabaWdbiaadAfapaWaaSbaaSqaa8qa \% caWG0bGaamiAaiaacYcacaaIXaGaaGimaiaadAfaa8aabeaaaOqaa8 \% qacaWGsbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGH \% RaWkcaaIYaGaaiOlaiaaiwdaaaaaaa!447D! 2 = \frac{{{V_{th,10V}}}}{{{R_{th}} + 2.5}}\% MathType!End!2!1!

%MathType!Translator!2!1!LaTeX.tdl!LaTeX2.09andlater!%MathType!MTEF!2!1!+%feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn%hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr%4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9LqJc9%vqaqpepm0xbba9pwe9Q8fs0yqaqpepae9pg0FirpepeKkFr0xfrx%frxb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8%qacqGHshI3daWcaaWdaeaapeGaaG4maaWdaeaapeGaaGOmaaaacqGH%9aqpdaWcaaWdaeaapeGaamOua8aadaWgaaWcbaWdbiaadshacaWGOb%aapaqabaGcpeGaey4kaSIaaGOmaiaac6cacaaI1aaapaqaa8qacaWG%sbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGHRaWkca%aIXaaaaaaa!469D!32=Rth+2.5Rth+1%MathType!End!2!1!\% MathType!Translator!2!1!LaTeX.tdl!LaTeX 2.09 and later! \% MathType!MTEF!2!1!+- \% feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn \% hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr \% 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq-Jc9 \% vqaqpepm0xbba9pwe9Q8fs0-yqaqpepae9pg0FirpepeKkFr0xfr-x \% fr-xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaaeaaaaaaaaa8 \% qacqGHshI3daWcaaWdaeaapeGaaG4maaWdaeaapeGaaGOmaaaacqGH \% 9aqpdaWcaaWdaeaapeGaamOua8aadaWgaaWcbaWdbiaadshacaWGOb \% aapaqabaGcpeGaey4kaSIaaGOmaiaac6cacaaI1aaapaqaa8qacaWG \% sbWdamaaBaaaleaapeGaamiDaiaadIgaa8aabeaak8qacqGHRaWkca \% aIXaaaaaaa!469D! \Rightarrow \frac{3}{2} = \frac{{{R_{th}} + 2.5}}{{{R_{th}} + 1}}\% MathType!End!2!1!

⇒ Rth = 2 Ω

Vth,10 V = 3 (2 + 1) = 9 V

Note than it is a nonreciprocal two port network thevenin voltage seen at port B depends on the voltage connected at port A. therefore we took subscript Vth,10 V . This is thevenin voltage only when 10 V source is connected at input port A. If the voltage connected to port A is different, then thevenin voltage will be different. However, Thevenin’s resistance remains same. Now, the circuit is

For RL = 7 Ω 

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62

In the circuit show, the three voltmeter readings are V1 = 220 V, V2 = 122 V, V3 = 136 V.

The power factor of the load is

  1. ((a))

    0.45

  2. ((b))

    0.50

  3. ((c))

    0.55

  4. ((d))

    0.60

Show Answer
Answer: ((a))

0.45

By taking V1, V2, V3 all are phasor voltages.

V1 = V2 + V3

⇒ V1 = V2 ∠0° + V3 ∠θ

V1 = V2 + V3 cos θ + j V3 sin θ

V1 = (V2 + V3 cos θ) + j V3 sin θ

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cosθ = 0.45

63

In the circuit show, the three voltmeter readings are V1 = 220 V, V2 = 122 V, V3 = 136 V.

If RL = 5 Ω, the approximate power consumption in the load is

  1. ((a))

    700 W

  2. ((b))

    750 W

  3. ((c))

    800 W

  4. ((d))

    850 W

Show Answer
Answer: ((b))

750 W

By taking V1, V2, V3 all are phasor voltages.

V1 = V2 + V3

⇒ V1 = V2 ∠0° + V3 ∠θ

V1 = V2 + V3 cos θ + j V3 sin θ

V1 = (V2 + V3 cos θ) + j V3 sin θ

V1=(V2+V3cosθ)2+(V3sinθ)2\left| {{V_1}} \right| = \sqrt {{{\left( {{V_2} + {V_3}\cos \theta } \right)}^2} + {{\left( {{V_3}\sin \theta } \right)}^2}}

220=(122+136cosθ)2+(136sinθ)2220 = \sqrt {{{\left( {122 + 136\cos \theta } \right)}^2} + {{\left( {136\sin \theta } \right)}^2}}

⇒ cosθ = 0.45

VRL = V3 cos θ = 136 × 0.45 = 61.2 V

Power absorbed in RL

PL=VRL2RL=(61.2)25=750;W{P_L} = \frac{{V_{RL}^2}}{{{R_L}}} = \frac{{{{\left( {61.2} \right)}^2}}}{5} = 750;W

The transfer function of a compensator is given as

Gc(S)=s+as+bG_c(S)=\frac{s+a}{s+b}

64

Gc(s) is a lead compensator if

  1. ((a))

    a = 1, b = 2

  2. ((b))

    a = 3, b = 2

  3. ((c))

    a = -3, b = -1

  4. ((d))

    a = 3, b = 1

Show Answer
Answer: ((a))

a = 1, b = 2

Concept:

The general expression for a lead compensator is;

G(s)=(α)(1+Ts)(1+αTs)G\left( s \right)=\frac{\left( \alpha \right)\left( 1+Ts \right)}{\left( 1+\alpha Ts \right)}

And for a lead compensator α < 1

Analysis:

Given lead compensator expression is;

Gc(s)=k(s+a)(s+b){{G}_{c}}\left( s \right)=\frac{k\left( s+a \right)}{\left( s+b \right)}

On comparing it with the standard expression we get;

T=1a ,  αT=1bT=\frac{1}{a}~,~~\alpha T=\frac{1}{b}

αa=1bα=ab\Rightarrow \frac{\alpha }{a}=\frac{1}{b}\Rightarrow \alpha =\frac{a}{b}

⇒ a < b

Only two options are valid as per the above condition, options 1 and 3

But we can't go with option 3, because for lead compensator zero is near to the origin compared to pole.

Hence, a = 1, b = 2

65

The phase of the above lead compensator is maximum at

  1. ((a))

    √2 rad/s

  2. ((b))

    √3 rad/s

  3. ((c))

    √6 rad/s

  4. ((d))

    1/√3 rad/s

Show Answer
Answer: ((a))

√2 rad/s

Maximum phase at frequency

 ωm=1Tα\rm {\omega _m} = \frac{1}{{T\sqrt \alpha }}   (for Gc(s)=1+sT1+αsT;α<1)\rm \left( {{\rm{for}}\ {G_c}\left( s \right) = \frac{{1 + sT}}{{1 + \alpha sT}};\alpha < 1} \right)

Gc(s)=s+1s+2=1+s1+0.5s\rm {G_c}\left( s \right) = \frac{{s + 1}}{{s + 2}} = \frac{{1 + s}}{{1 + 0.5s}}

Comparing T=1,αT=0.5\rm T = 1, αT = 0.5

α=0.5\rm α = 0.5

ωm=110.5=2 rad/sec\rm {\omega _m} = \frac{1}{{1\sqrt {0.5} }} = \sqrt 2\ {\rm{rad}}/{\rm{sec}}

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