Well, that was very interesting and well done. But I assume that turn analysis was based on neither gaining nor losing altitude in the turn. Losing altitude would decrease the G load required. And of course gaining altitude would enable a yo-yo maneuver, which I do not think was done in WWII.,
As for stall warning, the A-7D had a problem that if it stalled and did not enter a spin but instead something called a "post stall gyration" and the pilot applied normal spin recovery technuqies, he would never come out of it. The answer they came up with was to add a flap that was automatically deployed when a little black box (light green actually) detected the appropriate combination of static and ram air pressures. We were considering a version of that box to replace the original supersonic fuel transfer switch on the F-106A. I don't know if they added a flap to the A-7D or used the original flaps. In any case, we had so much trouble with the TF-41 engine that everyone was relieved to get the A-10.