How to Calculate Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle?
Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle calculator uses Pressure Coefficient = (2*Deflection Angle)/(sqrt(Mach Number^2-1)) to calculate the Pressure Coefficient, The Supersonic expression for pressure coefficient on surface with local deflection angle formula is defined as the ratio of deflection angle to the square root of free-stream Mach number minus 1. Pressure Coefficient is denoted by Cp symbol.
How to calculate Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle using this online calculator? To use this online calculator for Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle, enter Deflection Angle (θdef) & Mach Number (Mr) and hit the calculate button. Here is how the Supersonic Expression for Pressure Coefficient on Surface with Local Deflection Angle calculation can be explained with given input values -> 0.387836 = (2*0.19)/(sqrt(1.4^2-1)).