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At a static temperature of \( 250 \) K, the flow speed corresponding to \( M = 0.3 \) is nearest to

  • A.75 m/s
  • B.120 m/s
  • C.95 m/s
  • D.102 m/s

Answer: C

First the speed of sound: \( \sqrt{1.4 \times 287 \times 250} = \sqrt{100\,450} = 316.9 \) m/s. Then \( 0.3 \times 316.9 = 95.1 \) m/s. The colder air gives a lower threshold speed than the 102 m/s that applies at sea level, so compressibility sets in at a lower true airspeed at altitude.

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