> This would be hard to model using lookup tables, but it might be possible > using JSBSim functions and a table or tables, together. Could be > fun. I need > to think about this one. The first idea that comes to mind is that if the > aircraft speed minus the yaw rate times some characteristic lateral length > (span/2?) falls below the stall speed, then a rolling moment would be > generated - maybe a yawing moment, too. > > Jon
We might also calculate alpha at a few points along the wing and key off of that (partially) for roll and yaw moment deltas... Jon _______________________________________________ Flightgear-devel mailing list Flightgear-devel@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/flightgear-devel
