Simple Input File for Steady-State Viscous Flow

0.84
3.06
0.0
11.7
460.0
0
-1.0
0
0.5255
0.667
1.0
0.0
0.0
0.0
0
1
-150.0
50
150.0
5.0
0.0
1.0
0
0.3
500
-3.0
0
0
1500
0
3
1
0.5
0.05
0.001
0.
50
75
100
1500
2
0
0
2
1
1
1
3
0
0.0
10
0
0
0
0
0.
0.

This is a typical USM3D input file for a standard computation of a transonic aircraft with no engines. RED denotes the primary parameters that will require attention from the user. The remaining parameters can generally remain unchanged.