How to Calculate Pressure ratio of Blunt-nosed cylinder (first approximation):?
Pressure ratio of Blunt-nosed cylinder (first approximation): calculator uses pressure ratio=0.067*(Mach Number^2)*sqrt(Drag Coefficient)/(Distance from X-axis/Diameter ) to calculate the pressure ratio, Pressure ratio of Blunt-nosed cylinder (first approximation): formula is defined as interrelation between drag coefficient, mach number at infinity, distance from the tip of the slab and base diameter. pressure ratio and is denoted by Rp symbol.
How to calculate Pressure ratio of Blunt-nosed cylinder (first approximation): using this online calculator? To use this online calculator for Pressure ratio of Blunt-nosed cylinder (first approximation):, enter Mach Number (M), Drag Coefficient (C_{D}), Distance from X-axis (y) and Diameter (d) and hit the calculate button. Here is how the Pressure ratio of Blunt-nosed cylinder (first approximation): calculation can be explained with given input values -> 670 = 0.067*(1^2)*sqrt(100)/(0.01/10).