RE: Stall Question
This is related to his question, and not simply banter!
I guess my point is this; When a wing-any wing-is put at a steep enough angle, the airflow over the top of the wing(whether perfectly laminar or not) is disturbed to the point that it no longer works to create lift. This is why the military still uses washout in their wings still today.
As I recall, the gentleman said he already checked for lateral balance, and checked his elevator halves, as well as tinkered with CG, none of which helped him any. What else could it be?
The issue here is that this problem was so frustrating to me, when no one would even try to explain what in the world was going on. And I had access to many people who competed in major events(TOC for ex.) as well as design the airplanes when I lived in CO, and when I approached them, even though they knew how to fix the problem, refused to help! I hate to see it when other people go through that too. This is why I'm so passionate about this topic. It is SOO important to understand if you want success!