Pick out the correct statement pertaining to the flow through a converging-diverging tube ?

Correct answer: B. No shock wave develops in the tube when the Mach number at exit is greater than unity

  • A. The value of Mach number is always unity at the throat
  • B. No shock wave develops in the tube when the Mach number at exit is greater than unity
  • C. Throughout the converging portion of the tube, the density increases in the downstream
  • D. direction
  • E. None of these

Explanation

Mach number equals unity at the throat only when the nozzle is choked, not in every case. Under the usual one-dimensional nozzle model, a supersonic exit indicates that no normal shock has occurred inside the tube, making B the intended correct statement.

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