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Aerodynamics
Mach Number Ahead of Expansion Fan in Oblique Shock and Expansion Waves Formulas
Mach Number Ahead of Expansion Fan is the Mach number of the upstream flow. And is denoted by M
e1
.
Oblique Shock and Expansion Waves formulas that make use of Mach Number Ahead of Expansion Fan
f
x
Pressure Ratio across Expansion Fan
Go
f
x
Temperature Ratio across Expansion Fan
Go
f
x
Pressure behind Expansion Fan
Go
f
x
Temperature behind Expansion Fan
Go
f
x
Forward Mach Angle of Expansion Fan
Go
f
x
Prandtl Meyer Function at Upstream Mach Number
Go
f
x
Flow Deflection Angle due to Expansion Wave
Go
FAQ
What is the Mach Number Ahead of Expansion Fan?
Mach Number Ahead of Expansion Fan is the Mach number of the upstream flow.
Can the Mach Number Ahead of Expansion Fan be negative?
{YesorNo}, the Mach Number Ahead of Expansion Fan, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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