Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number evaluator uses Pressure Coefficient = 4/(Specific Heat Ratio+1)*(sin(Wave Angle))^2 to evaluate 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 evaluate Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number using this online evaluator? To use this online evaluator for Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number, enter Specific Heat Ratio (Y) & Wave Angle (β) and hit the calculate button.