How to Calculate Temperature given Dynamic Pressure and Mach Number?
Temperature given Dynamic Pressure and Mach Number calculator uses Static Temperature = (2*Dynamic Pressure)/(Ambient Air Density*Mach Number^2*Specific Gas Constant*Heat Capacity Ratio) to calculate the Static Temperature, Temperature given Dynamic Pressure and Mach Number is a formula used in aerodynamics to determine the temperature of a gas under specific condition. Static Temperature is denoted by T symbol.
How to calculate Temperature given Dynamic Pressure and Mach Number using this online calculator? To use this online calculator for Temperature given Dynamic Pressure and Mach Number, enter Dynamic Pressure (q), Ambient Air Density (ρ), Mach Number (M), Specific Gas Constant (R) & Heat Capacity Ratio (Y) and hit the calculate button. Here is how the Temperature given Dynamic Pressure and Mach Number calculation can be explained with given input values -> 0.044443 = (2*10)/(1.225*8^2*4.1*1.4).