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SOLVED: For a given airfoil, the critical Mach number is 0.8. Calculate the value of P/Pat the minimum pressure point at this freestream Mach number. Note: the critical pressure coefficient is 2Cp * (
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Physics Formulae on X: "Today's formula of the day: The Definition of the Mach Number The Mach number of a moving object is the ratio of the speed of that object to
Is this formula correct, RAT = SAT + (Recovery Factor * (Mach Number^2))? - Quora
