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

ALL or blank
Results are output for all points. 2
NO
Results are not output.
SID
Identification number of a SET case control entry.
If a set ID is specified, results are output only for elements listed in that set.

Comments

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