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

3.11.2 arsolmw - Oblique shock relations given M1   and δ
SUBROUTINE AR11AA(G,M,D,RESULT,IERR)
  DOUBLE PRECISION G, M, D, RESULT(10)
  INTEGER IERR

Compute the oblique shock relations given a mach number M and the wave angle δ .

Performance
Fixed

Arguments

G - REAL

ENTRY: Specific heat constant γ .

M - REAL

ENTRY: Mach number M  ≥1
 1  .

D - REAL

ENTRY: Wave angle 0< δ<90  .

RESULT - ARRAY OF REAL

EXIT: Array with result properties as described in  9.

IERR - INTEGER

EXIT: (optional) Return status code.

Status codes

-1

Specific heat ratio γ≤ 1  .

-2

Given M1   out of range.

-3

Given δ out of range.