arscomw - Conical flow given M and δ

Compressible Flow Subroutine Library
Programming Reference Manual
Version 1.0 DD-00008-110

SUBROUTINE AR17AA(G,M,W,RESULT,IERR)
  DOUBLE PRECISION G, M, W, RESULT(3)
  INTEGER IERR

Solve the conical flow given a mach number $M$ and wave angle $δ$ .

Performance
Iterative

Arguments


Argument	Intent	Description

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

Status codes