QuizMaster

Question: A closed cycle gas turbine consists of a
[A].

compressor

[B].

heating chamber

[C].

cooling chamber

[D].

all of these

Answer: Option D

Explanation:

No answer description available for this question.

Question: An open cycle gas turbine works on the same cycle as that of a closed cycle gas turbine.
[A].

Yes

[B].

No

Answer: Option A

Explanation:

No answer description available for this question.

Question: A closed cycle gas turbine works on
[A].

Carnot cycle

[B].

Rankine cycle

[C].

Ericsson cycle

[D].

Joule cycle

Answer: Option D

Explanation:

No answer description available for this question.

Question: Gas turbine as compared to internal combustion engine
[A].

can be driven at a very high speed

[B].

produces uniform torque

[C].

has more efficiency

[D].

all of these

Answer: Option D

Explanation:

No answer description available for this question.

Question: Gas turbine as compared to steam turbine
[A].

requires less space for installation

[B].

has compressor and combustion chamber

[C].

has less efficiency

[D].

all of these

Answer: Option D

Explanation:

No answer description available for this question.

Question: In a gas turbine, air is obtained from the atmosphere and compressed in an air compressor.
[A].

True

[B].

False

Answer: Option A

Explanation:

No answer description available for this question.

Question: The basic principle of the rocket propulsion is the same as that of jet propulsion.
[A].

Yes

[B].

No

Answer: Option A

Explanation:

No answer description available for this question.

Question: Only rocket engines can be propelled to space because
[A].

they can generate very high thrust

[B].

they have high propulsion efficiency

[C].

these engines can work on several fuels

[D].

they are not air-breathing engines

Answer: Option D

Explanation:

No answer description available for this question.

Question: Which of the following statement is correct relating to rocket engines ?
[A].

The combustion chamber in a rocket engine is directly analogous to the reservoir of a super sonic wind tunnel

[B].

The stagnation conditions exist at the combustion chamber

[C].

The exit velocities of exhaust gases are much higher than those in jet engine

[D].

all of the above

Answer: Option D

Explanation:

No answer description available for this question.

Question: A rocket works with maximum overall efficiency when air-craft velocity is __________ the jet velocity.
[A].

equal to

[B].

one-half

[C].

double

Answer: Option B

Explanation:

No answer description available for this question.