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Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines

Exercise : Compressors, Gas Dynamics and Gas Turbines - Section 1
36.
The actual volume of air delivered by a compressor, When reduced to the normal temperature and pressure conditions is called compressor capacity.
Yes
No
Answer: Option
Explanation:
No answer description is available. Let's discuss.
37.
The compression ratio in a gas turbine is
4
1
9
12
Answer: Option
Explanation:
No answer description is available. Let's discuss.
38.
Intercooling in compressors results in saving of power in compressing given volume of air to a given pressure.
Correct
Incorrect
Answer: Option
Explanation:
No answer description is available. Let's discuss.
39.
Only rocket engines can be propelled to space because
they can generate very high thrust
they have high propulsion efficiency
these engines can work on several fuels
they are not air-breathing engines
Answer: Option
Explanation:
No answer description is available. Let's discuss.
40.
The maximum combustion pressure in gas turbine is __________ as compared to I.C. engine.
more
less
Answer: Option
Explanation:
No answer description is available. Let's discuss.
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