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Compressibility effects in air are generally regarded as negligible below a Mach number of about

  • A.Zero point nine
  • B.One point five
  • C.Three point zero
  • D.Zero point three

Answer: D

Below roughly Mach 0.3 the density change through the flow is only a few per cent, so the incompressible equations are accurate enough for most purposes. Above that the error grows quickly and compressible relations must be used.

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