Originally Posted by
pstaney
Other way around. Center of pressure will change with mach and aoa. It is aerodynamic center that really doesn't change, theoretically calculated at exactly 25% MAC, but typically between 23 and 27%. There was a very informative thread on this a year or 2 ago. Keith Williams explained it well.
Thanx =)
I tried to find the thread but was unable to do so by searching for posts with his name...
