> > There might be a yaw rate effect too. When the aircraft is yawing, > > the wingtip going "back" also sees a higher AoA and will drop if it is > > past the stall. Same deal. The snap roll needs a stalled "down" > > wingtip to get the divergence, in any case. > > That makes sense -- thanks.
There's also the shadowing of an inboard portion of one wing as beta gets larger. Don't know if that is part of the effect, tho'. Jon
smime.p7s
Description: application/pkcs7-signature
