arscoms - Conical flow given M and θ

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

void arscoms(double g, double m, double s, double result[3], int *ierr);

Solve the conical flow given a mach number $M$ and deflection surface angle $θ$ .

Performance
Iterative

Arguments


Argument	Intent	Description

g	in	Specific heat constant $γ$ .
m	in	Mach number $M ≥1$ .
s	in	Deflection surface angle $0<θ <90$ .
result	out	Array with result properties as described in 15.
ierr	out	(optional) Return status code

Status codes