How to Calculate Pressure Ratio when Mach becomes Infinite?
Pressure Ratio when Mach becomes Infinite calculator uses Pressure Ratio = (2*Specific Heat Ratio)/(Specific Heat Ratio+1)*(Mach Number*sin(Wave Angle))^2 to calculate the Pressure Ratio, Pressure Ratio when Mach becomes Infinite formula is defined as a measure of the ratio of total pressure behind an oblique shock wave to the total pressure in front of it, used to analyze the behavior of supersonic flows in aerodynamics and aerospace engineering. Pressure Ratio is denoted by rp symbol.
How to calculate Pressure Ratio when Mach becomes Infinite using this online calculator? To use this online calculator for Pressure Ratio when Mach becomes Infinite, enter Specific Heat Ratio (Y), Mach Number (M) & Wave Angle (β) and hit the calculate button. Here is how the Pressure Ratio when Mach becomes Infinite calculation can be explained with given input values -> 18.10502 = (2*1.6)/(1.6+1)*(8*sin(0.5))^2.