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Which law states that for an adiabatic and steady flow, the Mach number can not increase across a normal shock wave?
Question

Which law states that for an adiabatic and steady flow, the Mach number can not increase across a normal shock wave?

A.

Rankine-Hugoniot relation

B.

Second law of thermodynamics

C.

Rayleigh line

D.

First law of thermodynamics

Correct option is A

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