Compressors, Gas Turbines And Jet Engines MCQ Questions & Answers

Section 1 Section 2 Section 3 Section 4 Section 5

1.
The compression ratio for the compressor is always _________ unity.

A. Equal to

B. Less than

C. More than

D. None of these

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2.
The hottest point in a gas turbine is

A. At the base

B. At the tip

C. In the center

D. Between ~ to i of the blade height

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3.
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

A. Higher

B. Lower

C. Equal

D. Can't be compared

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4.
The maximum temperature in a gas turbine is

A. 200°C

B. 500°C

C. 700°C

D. 1000°C

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5.
In a jet propulsion

A. The propulsive matter is ejected from within the propelled body

B. The propulsive matter is caused to flow around the propelled body

C. Its functioning does not depend upon presence of air

D. None of the above

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Compressors, Gas Turbines And Jet Engines MCQ Questions & Answers | Mechanical Engineering

1. The compression ratio for the compressor is always _________ unity.

Answer & Solution

2. The hottest point in a gas turbine is

Answer & Solution

3. Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

Answer & Solution

4. The maximum temperature in a gas turbine is

Answer & Solution

5. In a jet propulsion

Answer & Solution

Read More Section(Compressors, Gas Turbines and Jet Engines)

1.
The compression ratio for the compressor is always _________ unity.

2.
The hottest point in a gas turbine is

3.
Temperature of gases at end of compression as compared to exhaust gases in a gas turbine is

4.
The maximum temperature in a gas turbine is

5.
In a jet propulsion