arsnsm1 - Normal shock relations given M1n

Compressible Flow Subroutine Library
Programming Reference Manual
Version 1.0 DD-00008-010

void arsnsm1(double g, double m, double result[5], int *ierr);

Compute the normal shock relations given the upstream mach number $M1n$ .

Performance
Fixed

Arguments


Argument	Intent	Description

g	in	Specific heat constant $γ$ .
m	in	Upstream number $M1n ≥1$ .
result	out	Array with result properties as described in 8.
ierr	out	(optional) Return status code

Status codes