How to Calculate Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite?
Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite calculator uses Pressure coefficient=(4/(Specific Heat Ratio+1))*(sin(Wave angle))^2 to calculate the Pressure coefficient, The Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite formula is interrelation between specific heat ratio and sin of wave angle. Pressure coefficient and is denoted by C_{p} symbol.
How to calculate Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite using this online calculator? To use this online calculator for Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite, enter Specific Heat Ratio (γ) and Wave angle (β) and hit the calculate button. Here is how the Exact relation for pressure coefficient behind an oblique shock wave when Mach no. tends to infinite calculation can be explained with given input values -> 0.04639 = (4/(1.6+1))*(sin(10))^2.