How to Calculate Aerodynamic Heating Equation for Stanton number?
Aerodynamic Heating Equation for Stanton number calculator uses Stanton Number = Local Heat Transfer Rate/(Static Density*Static Velocity*(Adiabatic Wall Enthalpy-Wall Enthalpy)) to calculate the Stanton Number, The Aerodynamic Heating Equation for Stanton number formula is defined as the interrelation between static density, the static velocity of the fluid, Stanton number, and the wall enthalpies. Stanton Number is denoted by St symbol.
How to calculate Aerodynamic Heating Equation for Stanton number using this online calculator? To use this online calculator for Aerodynamic Heating Equation for Stanton number, 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 Aerodynamic Heating Equation for Stanton number calculation can be explained with given input values -> 0.171898 = 12000/(98.3*8.8*(102-99.2)).