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Fluid Mechanics
Mach Number in Hypersonic Flow Formulas
Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound. And is denoted by M.
Formulas to find Mach Number in Hypersonic Flow
f
x
Mach Number with Fluids
Go
Hypersonic Flow formulas that make use of Mach Number
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Exact Pressure Ratio
Go
f
x
Exact Density Ratio
Go
f
x
Pressure Ratio when Mach becomes Infinite
Go
f
x
Dynamic Pressure for given Specific Heat Ratio and Mach Number
Go
f
x
Pressure Coefficient behind Oblique Shock Wave
Go
f
x
Temperature Ratio when Mach Becomes Infinite
Go
f
x
Exact Normal Shock Wave Maximum Coefficient of Pressure
Go
f
x
Pressure Coefficient for Blast Wave Theory
Go
f
x
Pressure Coefficient for Blast Wave Theory at Very High Values of Mach
Go
f
x
Mach Wave behind Shock with Mach Infinity
Go
f
x
Local Shock Velocity Equation
Go
f
x
Detachment Distance of Sphere Cone Body Shape
Go
f
x
Nose Radius of Sphere Cone
Go
f
x
Detachment Distance of Cylinder Wedge Body Shape
Go
f
x
Nose Radius of Cylinder-Wedge
Go
f
x
Hypersonic Similarity Parameter
Go
List of variables in Hypersonic Flow formulas
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x
Fluid Velocity
Go
f
x
Specific Heat Ratio
Go
f
x
Universal Gas Constant
Go
f
x
Final Temperature
Go
FAQ
What is the Mach Number?
Mach number is a dimensionless quantity representing the ratio of flow velocity past a boundary to the local speed of sound.
Can the Mach Number be negative?
{YesorNo}, the Mach Number, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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