Critical pressure ratio for choked flow in a nozzle Let p1 be the inlet (stagnation) pressure and p2 the throat static pressure at choking. Express the critical pressure ratio (p2/p1) in terms of the ratio of specific heats γ. Choose the correct expression.

Mechanical Engineering Steam Nozzles and Turbines Difficulty: Medium
Choose an option
  • A
    (2/(γ + 1))^(γ/(γ − 1))
  • B
    (γ + 1)/(γ − 1)
  • C
    (2γ/(γ + 1))^(1/(γ − 1))
  • D
    (γ − 1)/(γ + 1)

Answer

Correct Answer: (2/(γ + 1))^(γ/(γ − 1))

Explanation

Concept/Approach

  • For isentropic flow of a perfect gas, the sonic (choked) condition at the throat gives (p2/p1)crit = (2/(γ + 1))γ/(γ − 1).
  • This is derived from the energy equation and isentropic relations at Mach = 1.

Final Answer(2/(γ + 1))^(γ/(γ − 1))

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