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Fluid Mechanics
Specific Heat Ratio in Hypersonic Flow Formulas
The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to the heat capacity at constant volume, important for understanding fluid behavior in hypersonic flows. And is denoted by Y.
Hypersonic Flow formulas that make use of Specific Heat Ratio
f
x
Wave Angle for Small Deflection Angle
Go
f
x
Parallel Upstream Flow Components after Shock as Mach Tends to Infinite
Go
f
x
Perpendicular Upstream Flow Components behind Shock Wave
Go
f
x
Exact Pressure Ratio
Go
f
x
Density Ratio when Mach Becomes Infinite
Go
f
x
Exact Density Ratio
Go
f
x
Pressure Ratio when Mach becomes Infinite
Go
f
x
Velocity of Sound using Dynamic Pressure and Density
Go
f
x
Pressure Coefficient behind Oblique Shock Wave
Go
f
x
Temperature Ratio when Mach Becomes Infinite
Go
f
x
Pressure Coefficient behind Oblique Shock Wave for Infinite Mach Number
Go
FAQ
What is the Specific Heat Ratio?
The Specific Heat Ratio is the ratio of the heat capacity at constant pressure to the heat capacity at constant volume, important for understanding fluid behavior in hypersonic flows.
Can the Specific Heat Ratio be negative?
{YesorNo}, the Specific Heat Ratio, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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