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What is the problem in solving flows with Mach numbers around and above 1?

(a) Mach number

(b) Compressibility

(c) Continuity

(d) Pressure

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The correct choice is (b) Compressibility

To elaborate: Flows with Mach numbers around and above 1 has the additional issue of compressibility. Air becomes compressible at higher speeds and the effects of compressibility also should be included while solving the problem.

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