Recent content by 121706s

Where can I find Lift and Drag Coefficients for NACA four-digit airfoils? I tried using XFOIL, but was rather frustrated with the whole menu setup Thanks for any help you can offer!

Just a note - the V-22 problems are being solved, and the newly modified aircraft works quite well.

I commonly use something called AML, which stands for %Angled Minus %Loaded (percent of laminae @ angle to load minus %laminae in line with load), at my workplace. A few days ago, a co-worker needed to know who was the the first person/company to use it. I did some research and I'm beginning...