Question

4. The inlet and exit areas if a simple- diverging inlet such as the one shown in Fig 6.10 are A 1.11 m and A 4.864 m. If the ambient air pressure is pa 100 kPa and the flight Mach number is 1.56, (a) (10 points) what is the "best" exit-plane pressure pe for the shock to be swallowed? Simple diverging inlet Kantrowitz-Donaldson inlet Ai Low back pressure Low back pressure M

Answer 1

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