Mechanical Engineering - Compressors, Gas Dynamics and Gas Turbines

Exercise : Compressors, Gas Dynamics and Gas Turbines - Section 2
16.
For perfect intercooling in a three stage compressor,
p1p2 = p3p4
p1p3 = p2p4
Answer: Option
Explanation:
No answer description is available. Let's discuss.

17.
A machine used to raise the pressure of air is called
gas turbine
I.C engine
compressor
air motor
Answer: Option
Explanation:
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18.
The overall efficiency of the compressed air system is the
ratio of shaft output of the air motor to the shaft input to the compressor
ratio of shaft input to the compressor to the shaft output of air motor
product of shaft output of air motor and shaft input to the compressor
none of the above
Answer: Option
Explanation:
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19.
In a jet engine, the compression varies as the square of the speed.
Correct
Incorrect
Answer: Option
Explanation:
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20.
In a single acting reciprocating air compressor, without clearance, the compression of air may be
isothermal
polytropic
isentropic
any one of these
Answer: Option
Explanation:
No answer description is available. Let's discuss.