I/O Options and Subcase Information Entry Used to request aerodynamic loads on aerodynamic control points.


AEROF = option


Argument Options Description
option <ALL, NO, SID>

Default = ALL

ALL or blank
Results are output for all boxes. 2
Results are not output.
Identification number of a SET case control entry.
If a set ID is specified, results are output only for elements listed in that set.


  1. This command is supported only for Aeroelastic Static Analysis.
  2. The SET command references box identification numbers.
  3. Output is in the units of force or moment.
  4. Only aerodynamic forces on boxes specified on the SET command will be output.
  5. The output is printed in the .trim ASCII file.