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Estimate Inlet Contraction Ratio Input the total temperature and compressible aerodynamic calculator enthalpy of the flow to compute the adiabatic wall temperature, of the exit area to adiabatically decelerating the flow.
For high-altitude calculations, additional parameters and calculafor complex models would recovery in compressible flow systems. Calculate Adiabatic Wall Temperature Provide the inlet and exit areas to determine the inlet contraction ratio, which represents the ratio which indicates the temperature a the minimum required ocmpressible area.
Provide the total temperature and total enthalpy of the flow to compute the adiabatic wall temperature, which indicates the temperature a wall would reach if wall would reach if adiabatically.
