How to Calculate Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number?
Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number calculator uses Pressure Coefficient = 4/(Specific Heat Ratio+1)*(sin(Wave Angle))^2 to calculate the Pressure Coefficient, The Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number formula is the interrelation between the specific heat ratio and sin of wave angle. Pressure Coefficient is denoted by Cp symbol.
How to calculate Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number using this online calculator? To use this online calculator for Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number, enter Specific Heat Ratio (Y) & Wave Angle (β) and hit the calculate button. Here is how the Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number calculation can be explained with given input values -> 0.122641 = 4/(1.6+1)*(sin(0.286))^2.