AEROF
I/O Options and Subcase Information Entry Used to request aerodynamic loads on aerodynamic control points.
Format
AEROF = option
Definitions
Argument | Options | Description |
---|---|---|
option | <ALL, NO, SID> Default = ALL |
|
Comments
- This command is supported only for Aeroelastic Static Analysis.
- The SET command references user identification numbers of boxes or body elements.
- Output is in the units of force or moment.
- Only aerodynamic forces on points specified on the SET command are output.
- The output is printed in the .trim ASCII file.