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Fluid Mechanics
Specific Heat Ratio in Hypersonic Flow Formulas
The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume. And is denoted by γ.
Hypersonic Flow formulas that make use of Specific Heat Ratio
f
x
Density before Shock Formation for Expansion Wave
Go
f
x
New Pressure after Shock Formation, Subtracted to Velocity for Expansion Wave
Go
f
x
Pressure Ratio for Unsteady Waves with Subtracted Induced Mass Motion for Expansion Waves
Go
f
x
Ratio of New and Old Temperature for Expansion Waves
Go
f
x
Temperature Ratio for Unsteady Expansion Wave
Go
f
x
Temperature Ratio for Unsteady Compression Waves
Go
f
x
New Pressure after Shock Formation for Compression Wave
Go
f
x
Density before Shock Formation for Compression Wave
Go
f
x
Pressure Ratio for Unsteady Waves
Go
f
x
Ratio of New and Old Temperature
Go
FAQ
What is the Specific Heat Ratio?
The Specific heat ratio of a gas is the ratio of the specific heat of the gas at a constant pressure to its specific heat at a constant volume.
Can the Specific Heat Ratio be negative?
{YesorNo}, the Specific Heat Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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