wrote on 7/23/2020 7:18 AM:
On Thursday, July 23, 2020 at 12:55:12 AM UTC-4, Tango Whisky wrote:
The procedure is push and hard rudder. Ther are situations where this is the only way out.

Stupid question: if you push to zero-G, wouldn't then the yaw caused by the "hard rudder" have zero rolling effect, since both wings have zero AOA, thus the differential airspeed doesn't matter?

Because the wing has dihedral, the yaw from left rudder will give the right wing
more AOA, and left wing less AOA. And vice versa, of course.

--
Eric Greenwell - Washington State, USA (change ".netto" to ".us" to email me)
- "A Guide to Self-Launching Sailplane Operation"
https://sites.google.com/site/motorg...ad-the-guide-1