Eduardo Fadul
Well-Known Member
Good morning to all
I'm evaluating a collegue Thesis and I have a question.
She was trying to determinated the MAC and Y Mac according to USAF - Datcom (Double-delta and cranked Wing page 2.2.2-4) however the values doesn't fit.
Doing the math it gives:
Mac of the whole wing = 7.8841 ft
Y mac = 16.866 ft
but doing the CAD that MAC lies around 20.13 ft onder: :ermm:
So I'd like to know it there is another way to determinate that MAC and Y Mac for double tapered wing.
Thanks in advance
I'm evaluating a collegue Thesis and I have a question.
She was trying to determinated the MAC and Y Mac according to USAF - Datcom (Double-delta and cranked Wing page 2.2.2-4) however the values doesn't fit.
Doing the math it gives:
Mac of the whole wing = 7.8841 ft
Y mac = 16.866 ft
but doing the CAD that MAC lies around 20.13 ft onder: :ermm:
So I'd like to know it there is another way to determinate that MAC and Y Mac for double tapered wing.
Thanks in advance