Adiabatic Wall Enthalpy in Boundary Layer Equations for Hypersonic Flow Formulas

The Adiabatic Wall Enthalpy is the total enthalpy of a gas at the wall of a hypersonic vehicle, considering the heat transfer and friction effects. And is denoted by h_aw. Adiabatic Wall Enthalpy is usually measured using the Joule per Kilogram for Specific Energy. Note that the value of Adiabatic Wall Enthalpy is always positive.

Formulas to find Adiabatic Wall Enthalpy in Boundary Layer Equations for Hypersonic Flow

fxAdiabatic Wall Enthalpy using Stanton NumberGo

Boundary Layer Equations for Hypersonic Flow formulas that make use of Adiabatic Wall Enthalpy

fxStanton Number for Hypersonic VehicleGo

fxLocal Heat Transfer Rate Calculation using Stanton NumberGo

fxStatic Density Equation using Stanton NumberGo

fxStatic Velocity using Stanton NumberGo

fxEnthalpy of Wall using Stanton NumberGo

List of variables in Boundary Layer Equations for Hypersonic Flow formulas

fx Local Heat Transfer Rate Go

fx Static Density Go

fx Static Velocity Go

fx Stanton Number Go

fx Wall Enthalpy Go

FAQ

What is the Adiabatic Wall Enthalpy?

The Adiabatic Wall Enthalpy is the total enthalpy of a gas at the wall of a hypersonic vehicle, considering the heat transfer and friction effects. Adiabatic Wall Enthalpy is usually measured using the Joule per Kilogram for Specific Energy. Note that the value of Adiabatic Wall Enthalpy is always positive.

Can the Adiabatic Wall Enthalpy be negative?

No, the Adiabatic Wall Enthalpy, measured in Specific Energy cannot be negative.

What unit is used to measure Adiabatic Wall Enthalpy?

Adiabatic Wall Enthalpy is usually measured using the Joule per Kilogram[J/kg] for Specific Energy. Joule per Gram[J/kg], Joule per Centigram[J/kg], Square Meter per Square Second[J/kg] are the few other units in which Adiabatic Wall Enthalpy can be measured.

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