Aerowerx
Well-Known Member
I have been comparing the Panknin and Culver equations for calculating the required twist of a swept tapered wing, as presented on the B2Streams website.
You would think that even though they use different methods that they would give similar results.
However, I noticed that with Panknin the required twist gets smaller as the sweep increases. But with Culver the twist gets bigger as the sweep increases.:ermm:
So, what's going on here? Or is this version of the Culver equation wrong?
You would think that even though they use different methods that they would give similar results.
However, I noticed that with Panknin the required twist gets smaller as the sweep increases. But with Culver the twist gets bigger as the sweep increases.:ermm:
So, what's going on here? Or is this version of the Culver equation wrong?
