Air at Mach 1.8 at an altitude of 8 km ISA, passes through a normal shockwave. a)...

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Mechanical Engineering

Air at Mach 1.8 at an altitude of 8 km ISA, passes through anormal shockwave.

a) Calculate the velocity of the flow in units of metres persecond after the shock wave.

b) Calculate the change in specific entropy across theshockwave. Make sure you

include the appropriate units in your answer.

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