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

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

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

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

include the appropriate units in your answer.

Solutions

Expert Solution

Hope explanation is clear. Do get back for any query.

Will appreciate feedback.

samet mamat answered 1 year ago

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