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Aerodynamics
Upstream Mach Normal to Oblique Shock in Oblique Shock and Expansion Waves Formulas
Upstream Mach Normal to Oblique Shock represents the Mach number’s component aligned with the shock wave’s normal direction. And is denoted by M
n1
.
Formulas to find Upstream Mach Normal to Oblique Shock in Oblique Shock and Expansion Waves
f
x
Component of Upstream Mach Normal to Oblique Shock
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Oblique Shock and Expansion Waves formulas that make use of Upstream Mach Normal to Oblique Shock
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x
Density Ratio across Oblique Shock
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f
x
Pressure Ratio across Oblique Shock
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f
x
Temperature Ratio across Oblique Shock
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f
x
Component of Downstream Mach Number Normal to Oblique Shock for given Normal Upstream Mach Number
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f
x
Density behind Oblique Shock for given Upstream Density and Normal Upstream Mach Number
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f
x
Pressure behind Oblique Shock for given Upstream Pressure and Normal Upstream Mach Number
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f
x
Temperature behind Oblique Shock for given Upstream Temperature and Normal Upstream Mach Number
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List of variables in Oblique Shock and Expansion Waves formulas
f
x
Mach Number Ahead of Oblique Shock
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f
x
Oblique Shock Angle
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FAQ
What is the Upstream Mach Normal to Oblique Shock?
Upstream Mach Normal to Oblique Shock represents the Mach number’s component aligned with the shock wave’s normal direction.
Can the Upstream Mach Normal to Oblique Shock be negative?
{YesorNo}, the Upstream Mach Normal to Oblique Shock, measured in {OutputVariableMeasurementName} {CanorCannot} be negative.
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