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

3.12.3 arsolls - Compute maximum wave and deflection surface angle that wil result in sonic downstream flow
SUBROUTINE AR12AB(G,M,RESULT,IERR)
  DOUBLE PRECISION G, M, RESULT(3)
  INTEGER IERR

Compute maximum wave and deflection surface angle that wil result in sonic downstream flow given a mach number M .

Performance
Fixed

Arguments

G - REAL

ENTRY: Specific heat constant γ .

M - REAL

ENTRY: Mach number M ≥1  .

RESULT - ARRAY OF REAL

EXIT: Array with result properties as described in  10.

IERR - INTEGER

EXIT: (optional) Return status code.

Status codes

-1

Specific heat ratio γ≤ 1  .

-2

Given M out of range.