Lift and Drag total force for complete model
I'm fresh new user of Caedium, I have activated PanelFlow and Exchange .
I have review the tutorial and particularly the DLR-F4 Wing Body calculation.
Can someone describe step by step how to include in new results the Total Lift and Drag and total Moment Mx, My, Mz?
Why this standard data are not calculated automatically? I'm used to an old university code and F and M are standard output on body and aero frame.
Caedium seems very powerful with fantastic view features.
Many thanks for your support on this.