Jan 4, 2004 #1 121706s Aerospace Dec 27, 2003 3 0 0 US 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!
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!
Jan 4, 2004 1 #2 hombre Aerospace Jun 24, 2003 29 0 0 US The best resource (and a book all aero's should own) is Theory of Wing Sections by Abbott and von Doenhoff. This book has all kinds of the information on NACA airfoils. Hombre Upvote 0 Downvote
The best resource (and a book all aero's should own) is Theory of Wing Sections by Abbott and von Doenhoff. This book has all kinds of the information on NACA airfoils. Hombre