And I stated that doing flight test stall stuff is risky. The post I replied to just made a blanket statement that doing stalls below 10K was risking the airframe...that's a BS statement.
I wasn't "sitting in the back seat", I was flying the Mustang. I was doing as instructed by Lee Lauderbach..he happens to be the highest time Mustang pilot in the world and is considered by the Warbird community as one of the best so tell him how reckless it was...I can assure you he knows a heck of a lot more about it than you do. <G>
How much high performance aircraft time do you have? What do you base your opinion on?
Of course, stalls and accelerated stalled are completely different.
I practiced stalls in a Grumman C-1A back in the 70s. Nose up a bit, pull off power until the stall shaker begins to raise hell. Then, ease the yoke forward and gently feed in some throttle. The C-1A had an airflow sensor on the upper side of the left wing's leading edge. Stall onset was sudden and there was almost no buffet to warn the pilot. Thus, the stall shaker was employed on the yoke itself. Recovery wasn't difficult and altitude loss wasn't great. Nonetheless, since the parent aircraft (S2F) performed its mission at low level, a fully developed stall could find one running out of altitude before recovery was completed. Thus, the stall shaker carried over to the C-1A. These aircraft were also equipped with a G Limiting valve that gradually added resistance to the yoke as G increased.
By the way, Bodhi restores Warbirds for a living.
My regards,
Widewing