How to Calculate Stanton Number for Hypersonic Vehicle?
Stanton Number for Hypersonic Vehicle calculator uses Stanton Number = Local Heat Transfer Rate/(Static Density*Static Velocity*(Adiabatic Wall Enthalpy-Wall Enthalpy)) to calculate the Stanton Number, Stanton Number for Hypersonic Vehicle is defined as the interrelation as local heat transfer, static density, and velocity of the fluid, adiabatic and wall enthalpy. Stanton Number is denoted by St symbol.
How to calculate Stanton Number for Hypersonic Vehicle using this online calculator? To use this online calculator for Stanton Number for Hypersonic Vehicle, enter Local Heat Transfer Rate (qw), Static Density (ρe), Static Velocity (ue), Adiabatic Wall Enthalpy (haw) & Wall Enthalpy (hw) and hit the calculate button. Here is how the Stanton Number for Hypersonic Vehicle calculation can be explained with given input values -> 0.405844 = 12000/(1200*8.8*(102-99.2)).