Description
Precision:
Ratio of specific heats | γ | |
Upstream Mach number | M1 |
Downstream Mach number | M2 | ||
Expansion angle (deg) | θ | ||
Temperature ratio | T2/T1 | ||
Pressure ratio | p2/p1 | ||
Upstream Mach angle (deg) | μ1 | ||
Downstream Mach angle (deg) | μ2 |
Setting M1 = 1.0 will give the Prandtl-Meyer function (as θ), or its inverse (as M2).