Example Input File for Steady-State Viscous Flow (PA Scheme)
0.84
3.06
0.0
11.7
460.0
0
-1.0
0.5255
0.667
1.0
0.0
0.0
0.0
0
1
1.0
500
50.0
5.0
15
-1.0
0.0
0
0.3
500
-3.0
0
0
1500
0
0
0
0.05
0.002
0
0
5.0
0
50
75
100
1500
2
0
0
0
2
1
1
1
2
0
0.0
0
0
1000
0
0
0
0
0.0
0.0
0
1
1
1
1
0.0
1
3
0
3
3
2
0
1
15
-1.0
0.03
1.0
500
50.0
3.0
0.009
-1.0e-20
-1.0e-20
1
0
0.92
1.0e+20
1.0e+20
0
-1
0.0
This is a typical USM3D input file for a standard, steady-state computation of a transonic aircraft.
The RED denotes the primary parameters that will require attention from the user and the GREEN denotes parameters specific to the PA scheme. The remaining parameters can generally remain unchanged.
Primary parameters:
xmach, alpha, beta, reue, tinf, sref, cref, bref, xmc, ymc, zmc, cfl1, iramp, cfl2, irest, limiter, limitert, lim_frz, ivisc, ncyc, cflt1, irampt, cflt2
Parameters specific to PA scheme:
nstage, nstagtrb, dtrbmax, nsd_gcr
