Jim Wilson writes: > The pitch angle seems to be way too high when at altitude (not > climbing), which of course would cause a decrease of airspeed and > power. The altitude starts to decrease smoothly as IAS passes > below 300knots...not in a "stall" fashion. This is running with > the default half full tanks. Just wondering if you're seeing this > as well on your 2.95.2 build.
Roskam's sample data for a 747-200 in cruise at 40,000ft gives these conditions: angle of attack: 2.4deg mach number: 0.9 TAS: 871fps (=516kt) weight: 636,636lb All the best, David -- David Megginson, [EMAIL PROTECTED], http://www.megginson.com/ _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
