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Aerodynamics
Rearward Mach Angle in Oblique Shock and Expansion Waves Formulas
Rearward Mach angle is the angle formed between the rearward Mach line and the downstream flow direction (parallel to the convex surface). And is denoted by μ
2
. Rearward Mach Angle is usually measured using the Degree for Angle. Note that the value of Rearward Mach Angle is always positive.
Formulas to find Rearward Mach Angle in Oblique Shock and Expansion Waves
f
x
Rearward Mach Angle of Expansion Fan
Go
List of variables in Oblique Shock and Expansion Waves formulas
f
x
Mach Number Behind Expansion Fan
Go
FAQ
What is the Rearward Mach Angle?
Rearward Mach angle is the angle formed between the rearward Mach line and the downstream flow direction (parallel to the convex surface). Rearward Mach Angle is usually measured using the Degree for Angle. Note that the value of Rearward Mach Angle is always positive.
Can the Rearward Mach Angle be negative?
No, the Rearward Mach Angle, measured in Angle cannot be negative.
What unit is used to measure Rearward Mach Angle?
Rearward Mach Angle is usually measured using the Degree[°] for Angle. Radian[°], Minute[°], Second[°] are the few other units in which Rearward Mach Angle can be measured.
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