arsptm - (Rayleigh-)Pitot relations given M

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

double arsptm(double g, double m, int *ierr);

Compute the Rayleigh-Pitot properties given a mach number $M$ .

Performance
Fixed

Arguments


Argument	Intent	Description

g	in	Specific heat constant $γ$ .
m	in	Mach number $M >0$ .
result	out	Array with result properties as described in 13.
ierr	out	(optional) Return status code

Status codes

Return Values
The pressure ratio $p0/p$ or $p02/p1$ or NAN on error.