Compressible Flow Subroutine Library
Programming Reference Manual
Version 1.0 DD-00008-110
3.11.8 arsolms - Oblique shock relations given M1   and θ
SUBROUTINE AR11AG(G,M,T,STRONG,RESULT,IERR)
  DOUBLE PRECISION G, M, T, RESULT(10)
  LOGICAL STRONG
  INTEGER IERR

Compute the oblique shock relations given the mach number M1   and the deflection surface angle θ .

Performance
Fixed

Arguments




Argument Intent

Description




g in

Specific heat constant γ .

d in

Density ratio M1 ≥1  .

t in

Deflection surface angle 0<θ <90  .

result out

Array with result properties as described in  9.

ierr out

(optional) Return status code




Status codes

-1

Specific heat ratio γ≤ 1  .

-2

Given M1   out of range.

-3

Given θ out of range.

-4

Calculation failed.