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Mechanical Engineering
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Compressors, Gas Dynamics and Gas Turbines
Comments
Question
The absolute pressure of air at the outlet of a compressor is called
Options
A. back pressure
B. critical pressure
C. discharge pressure
D. none of these
Correct Answer
discharge pressure
Compressors, Gas Dynamics and Gas Turbines problems
Search Results
1. The assumption made in two stage compression with intercooler is that
Options
A. there is no pressure drop in the intercooler
B. the compression in both the cylinders is polytropic
C. the suction and delivery of air takes place at constant pressure
D. all of the above
Show Answer
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Discuss
Correct Answer: all of the above
2. Standard air is the air at __________ and relative humidity of 36 percent.
Options
A. 0.1 bar and 20° C
B. 1 bar and 20° C
C. 0.1 bar and 40° C
D. 1 bar and 40° C
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Correct Answer: 1 bar and 20° C
3. The ratio of the isothermal power to the shaft power or brake power of the motor or engine required to drive the compressor is called overall isothermal efficiency.
Options
A. True
B. False
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Correct Answer: True
4. When the outlet angle from the rotor of a centrifugal compressor is more than 90°, then the blades are said to be
Options
A. forward curved
B. backward curved
C. radial
D. none of these
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Correct Answer: forward curved
5. In axial flow compressors, the flow of air is parallel to the axis of compressor.
Options
A. Correct
B. Incorrect
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Correct Answer: Correct
6. The air power of the compressor is also known as
Options
A. indicated power
B. brake power
C. frictional power
D. none of these
Show Answer
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Discuss
Correct Answer: indicated power
7. The speed of rotary air compressor is __________ as compared to reciprocating air compressor.
Options
A. high
B. low
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Correct Answer: high
8. A centrifugal compressor is an axial flow compressor.
Options
A. Correct
B. Incorrect
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Correct Answer: Incorrect
9. When air is to be compressed at a high pressure, then it is advantageous to use
Options
A. single stage compression
B. multi-stage compression without intercooling
C. multi-stage compression with intercooling
D. none of these
Show Answer
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Correct Answer: multi-stage compression with intercooling
10. The basic principle of the rocket propulsion is the same as that of jet propulsion.
Options
A. Yes
B. No
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Correct Answer: Yes
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