At which diameter we should design a supersonic after burning engine f – McqOptions

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1.	At which diameter we should design a supersonic after burning engine for a fighter which will have thrust at takeoff 150000 Unit and bypass ratio of 0.7.
A.	114.67 unit
B.	160.78 unit
C.	350.39 unit
D.	235.78 unit
Answer» B. 160.78 unit

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