Jim Wilson wrote: > The pitch angle seems to be way too high when at altitude (not > climbing) [...] But now I'm thinking that the real issue has to do > with the lift calculation. [...] 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.
My 2.95.2 build doesn't work. :) Yours does only because you played with the thresholds. I'd be really suspicious of any "solution" obtained under such circumstances. Let me find and fix the compiler dependant solution failure first, then we can worry about simulation issues. The lack of a clear "stall", however, is probably not a bug. Big planes don't experience the same kind of giant attitude change inside the stall that the little ones do, they just drop faster. The fact that it happens at 300 KIAS is a problem, but I'll put that to the solution failure until proven otherwise. Andy -- Andrew J. Ross NextBus Information Systems Senior Software Engineer Emeryville, CA [EMAIL PROTECTED] http://www.nextbus.com "Men go crazy in conflagrations. They only get better one by one." - Sting (misquoted) _______________________________________________ Flightgear-devel mailing list [EMAIL PROTECTED] http://mail.flightgear.org/mailman/listinfo/flightgear-devel
