[NineLine]

Originally Posted by Crumpp

Yeah you missed the fact it is the same airfoil selection and wing design

Engineering wise, they will have the same CLmax and lift distribution.

An anton does not stall at 87 mph and neither does a Dora.




If you know the basic relationship of Reynolds Number to CLmax....

It is a simple fact the higher Reynolds that the FW-190 series stalls at requires a higher CLmax.

I think maybe you missed a few facts at this point

[Crumpp+]

think maybe you missed a few facts at this point

By all means point them out!!!


Oh yeah...

You cannot....

You want the Focke Wulf investigations and comparative testing results??

Originally Posted by SiThSpAwN

I think maybe you missed a few facts at this point

Point them out please because your post does not make much sense.

It might be more productive for you to name what exactly you think is wrong?

[NineLine]

Originally Posted by Crumpp

Point them out please because your post does not make much sense.

It might be more productive for you to name what exactly you think is wrong?

I can start with resurrecting a post from a year ago that nobody but yourself seems to care about...