P5- Karman-Tsien compressibility correction formula for pressures in subsonic compressible flows $C_{p} = \frac{Sro}{B + \frac{M ^{2} Cpo}{( 1 + B ) 2}}, ? = 1 ? M_{?}^{2}$ $? = 1 ? M_{?}^{2}$ given in the form. Accordingly, at low Mach numbers (incompressible state), calculate the critical Mach number for an airfoil with the smallest pressure coefficient $Cpo = ? 0.5$ by applying the Karman-Tsien correction formula.

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P5- Karman-Tsien compressibility correction formula for pressures in subsonic compressible flows

C_{p} = \frac{Sro}{B + \frac{M ^{2} Cpo}{( 1 + B ) 2}}, ? = 1 ? M_{?}^{2}

? = 1 ? M_{?}^{2}

given in the form. Accordingly, at low Mach numbers (incompressible state), calculate the critical Mach number for an airfoil with the smallest pressure coefficient

Cpo = ? 0.5

by applying the Karman-Tsien correction formula.

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