The maximum propulsion efficiency of a turbojet is attained at around following speed
A. 550 km/hr
B. 1050 km/hr
C. 1700 km/hr
D. 2400 km/hr
Answer: Option D
Solution(By Examveda Team)
The maximum propulsion efficiency of a turbojet is attained at around following speed 2400 km/hrRelated Questions on Compressors, Gas Turbines and Jet Engines
The compression ratio for the compressor is always _________ unity.
A. Equal to
B. Less than
C. More than
D. None of these
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
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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