Physics, asked by ranishashree, 6 months ago

At a given point in a supersonic wind tunnel, the pressure and temperature are 5 x 104 N/m2 and 200 K, respectively. The total pressure at this point is 1.5 x 106 N/m2 . Calculate the local Mach number and total temperature.

Answers

Answered by navyasharma2607

1

Answer:

hiiii how r u please mark me as brain liest..........

Answered by nawazkhan69444

0

Explanation:

THIS QUESTION IS NOT UNDERSTAND.

WHICH CLASS QUESTION.

I AM IN CLASS 8.

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