> > No assumptions are made for the horizontal stabilizer, whether it is > all-moving, or is fixed with a movable surface. There is only a deflection > associated with the surface, and that is used to index into an aero table. I > am not quite sure what you need, or what you are referring to here. Using > properties, one could define just about anything they want to. Can you be > more descriptive about exactly what you want?
I would need: CLtail = f(alpha_tail, delta_elevator) where alpha_tail = alpha_aircraft + horizontal_stab_angle - Epsilon Some time ago I've been told that this can be done using the speedbrake property (indeed this is the way it is done in the 747 example) as if it were the stabilizer (only a matter of names); that's OK, but I only wonder whay there is no stabilizer property, or is it? I hope this time I was more descriptive. Thanks. ------------------------------------------------------------------------- This SF.net email is sponsored by: Splunk Inc. Still grepping through log files to find problems? Stop. Now Search log events and configuration files using AJAX and a browser. Download your FREE copy of Splunk now >> http://get.splunk.com/ _______________________________________________ Flightgear-devel mailing list Flightgear-devel@lists.sourceforge.net https://lists.sourceforge.net/lists/listinfo/flightgear-devel
