On 07/10/2007, Jon S. Berndt <[EMAIL PROTECTED]> wrote: > I looked at the configuration file for the Seneca II in flightgear cvs. It > appears to me (at least given the quick glance I took) that adverse aileron > yaw (Cnda) is turned off - the data is all zeros.
I'm not sure about the exact derivatives, but the real PA-28 and the 172 experience negligible adverse yaw in level cruise at bank angles under 20-30 degrees -- you can fly them with your feet flat on the floor and the slip-skid ball barely moves. In both, I think, it's the use of differential aileron deflections that does the trick. All the best, David ------------------------------------------------------------------------- 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
