An aircraft is flying with Mach 2.0. Calculate recovery temperature if ambient temperature is 305K. Assume recovery factor is 0.85.

A)
512.4K
B)
400°C
C)
253.2K
D)
100°C

Correct Answer :   512.4K


Explanation : Given, Mach number = 2.0, ambient temperature T1 = 305K
Assuming the recover factor as 0.85 and for such case,
Recovery temperature T2 = T1*(1+0.17*M²)
T2 = 305*(1+0.17*2*2) = 305*1.68 = 512.4K.