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Local Skin-Friction Coefficient in Boundary Layer Equations for Hypersonic Flow Formulas
Local Skin-Friction Coefficient specifies the fraction of the local dynamic pressure. And is denoted by C
f
.
Formulas to find Local Skin-Friction Coefficient in Boundary Layer Equations for Hypersonic Flow
f
x
Local Skin-Friction Coefficient
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Boundary Layer Equations for Hypersonic Flow formulas that make use of Local Skin-Friction Coefficient
f
x
Local Shear Stress at Wall
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f
x
Static Density Equation using Skin Friction Coefficient
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f
x
Static Velocity Equation using Skin Friction Coefficient
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List of variables in Boundary Layer Equations for Hypersonic Flow formulas
f
x
Shear Stress
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f
x
Static Density
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f
x
Static Velocity
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FAQ
What is the Local Skin-Friction Coefficient?
Local Skin-Friction Coefficient specifies the fraction of the local dynamic pressure.
Can the Local Skin-Friction Coefficient be negative?
{YesorNo}, the Local Skin-Friction Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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