arscoms - Conical flow given M and θ

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

SUBROUTINE AR17AB(G,M,S,RESULT,IERR)
  DOUBLE PRECISION G, M, S, RESULT(3)
  INTEGER 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