Discussion :: GATE Aeronautical Engineering
- Consider two engines P and Q. In P, the high pressure turbine blades are cooled with a bleed of 5% from the compressor after the compression process and in Q the turbine blades are not cooled. Comparing engine P with engine Q, which one of the following is NOT TRUE?
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A.
Turbine inlet temperature is higher for engine P
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B.
Specific thrust is higher for engine P
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C.
Compressor work is the same for both P and Q
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D.
Fuel flow rate is lower for engine P
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Answer : Option D
Explanation :
-NA-
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