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GATE 2022 AE – Question 25

Aerodynamics · Compressible flows: isentropic flow, normal and oblique shocks, Prandtl-Meyer flow, nozzles and diffusers · 1 mark · Multiple select

Across an oblique shock wave in a calorifically perfect gas,

  1. the stagnation enthalpy changes
  2. the stagnation entropy changes
  3. the stagnation temperature changes
  4. the speed of sound changes

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Show answer and explanation

Correct answer: (B) the stagnation entropy changes; (D) the speed of sound changes

Explanation

Across an **oblique shock** in a calorically perfect gas (steady, adiabatic):

(The stagnation pressure falls, which is the real loss caused by the shock.) Answer **B and D**.