Inverse of Density for Hypersonic Flow using Mach Number evaluator uses Inverse of Density = (2+(Specific Heat Ratio-1)*Mach Number^2*sin(Deflection Angle)^2)/(2+(Specific Heat Ratio+1)*Mach Number^2*sin(Deflection Angle)^2) to evaluate the Inverse of Density, The Inverse of density for hypersonic flow using Mach number formula is defined as the interrelation between the Mach number, specific heat ratio, and deflection angle. Inverse of Density is denoted by ϵ symbol.
How to evaluate Inverse of Density for Hypersonic Flow using Mach Number using this online evaluator? To use this online evaluator for Inverse of Density for Hypersonic Flow using Mach Number, enter Specific Heat Ratio (γ), Mach Number (M) & Deflection Angle (θd) and hit the calculate button.