A supersonic aircraft is designed to operate at 2.0M if thrust loss is – McqOptions

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1.	A supersonic aircraft is designed to operate at 2.0M if thrust loss is required to be less than 2% then determine the reference value of inlet pressure recovery. Given ram recovery Correction factor C is 1.2.
A.	95%
B.	99
C.	102
D.	70
Answer» B. 99

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