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))
Discussion & Comments