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Aerodynamics
Specific Heat Ratio in Normal Shock Wave Formulas
The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume. And is denoted by γ.
Normal Shock Wave formulas that make use of Specific Heat Ratio
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Relation between Mach Number and Characteristic Mach Number
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Mach Number behind Shock
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Velocity behind Normal Shock
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Stagnation Pressure behind Normal Shock by Rayleigh Pitot Tube formula
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Density behind Normal Shock given Upstream Density and Mach Number
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Static Pressure behind Normal Shock for given Upstream Pressure and Mach Number
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Static Temperature behind Normal Shock for given Upstream Temperature and Mach Number
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Static Enthalpy behind Normal Shock for given Upstream Enthalpy and Mach Number
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Shock Strength
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Density Ratio across Normal Shock
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Pressure Ratio across Normal Shock
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Temperature Ratio across Normal Shock
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Static Enthalpy Ratio across Normal Shock
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FAQ
What is the Specific Heat Ratio?
The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to heat capacity at constant volume.
Can the Specific Heat Ratio be negative?
{YesorNo}, the Specific Heat Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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