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| Fin Aeros Table |
Open the “Fin Aeros” table and see in the screen capture below that the Aeros for the Forward canard (F1) has been populated. Note the fin column headings end in _Fx x being the fin number.
The fin aeros summarizes the aero state of the fins and body separated from each other. For the fins this include Axial Drag, Normal Force Derivative, Center of Pressure and Roll Moment (Per Degree) roll damping and damping factors. The same is done for the body alone.
This table is also found in the "Aero Direct Input". It is the "Fin Alone" table.
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