Pressure Coefficient in Hypersonic Flow Formulas

The Pressure Coefficient is a dimensionless number that represents the relative pressure difference across a surface in fluid flow, indicating how pressure varies in different flow conditions. And is denoted by C_p.

Formulas to find Pressure Coefficient in Hypersonic Flow

fxCoefficient of Pressure Derived from Oblique Shock TheoryGo

fxPressure Coefficient behind Oblique Shock WaveGo

fxNon-Dimensional Pressure CoefficientGo

fxPressure Coefficient behind Oblique Shock Wave for Infinite Mach NumberGo

List of variables in Hypersonic Flow formulas

fx Wave Angle Go

fx Specific Heat Ratio Go

fx Mach Number Go

fx Change in Static Pressure Go

fx Dynamic Pressure Go

FAQ

What is the Pressure Coefficient?

The Pressure Coefficient is a dimensionless number that represents the relative pressure difference across a surface in fluid flow, indicating how pressure varies in different flow conditions.

Can the Pressure Coefficient be negative?

{YesorNo}, the Pressure Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.

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