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1. The main reason for adopting the axial flow compressors instead of centrifugal compressors in aircraft turbine is that:
(A): Starting torque for axial flow compressor is high
(B): The frontal area of axial flow compressor is considerably less
(C): The efficiency of middle speed range is higher
(D): Pressure ratio per stage is high
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kerala-psc
ASST-ENGINEER---MECHANICAL---TTP-LTD-ASST-ENGINEER---MECHANICAL---SFC-OF-KERALA-LTD
147/2015
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