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Fluid Mechanics
Pressure Coefficient in Hypersonic Flow Formulas
The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave. And is denoted by C
p
.
Formulas to find Pressure Coefficient in Hypersonic Flow
f
x
Pressure Coefficient Combined with Blast Wave for Shuttle at Angle of Attack
Go
f
x
Pressure Coefficient for Blunt-Nosed Plate
Go
f
x
Pressure Coefficient for Blunt-Nosed Cylinder
Go
f
x
Pressure Coefficient Combined with Blast Wave for Shuttle
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
List of variables in Hypersonic Flow formulas
f
x
Distance from X-Axis
Go
f
x
Length of Shuttle
Go
f
x
Angle of Attack
Go
f
x
Drag Coefficient
Go
f
x
Distance from Y-Axis
Go
f
x
Diameter 1
Go
f
x
Distance from Nose Tip to Required Base Diameter
Go
f
x
Diameter
Go
f
x
Specific Heat Ratio
Go
f
x
Mach Number
Go
f
x
Pressure Ratio
Go
FAQ
What is the Pressure Coefficient?
The Pressure Coefficient is a dimensionless quantity used to describe the ratio of dynamic pressure to static pressure in a blast wave.
Can the Pressure Coefficient be negative?
{YesorNo}, the Pressure Coefficient, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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