Mr. Chen Zicheng 0 Report post Posted July 21, 2016 Hey guys: Any one has the info of naca66 a=0.8 mean camer line? On many occasions, I have run into this type of curve. As we know, many types of naca66 are included in CAESES, just don't know which one is "naca66 a=0.8 mean camer line" Best Regards,Chen Share this post Link to post Share on other sites
Mr. Claus Abt 14 Report post Posted July 21, 2016 If I recall correctly such a meanline distribution creates constant lift of 80% of the chord, then dropping linearly to zero at 100%. You can find some details in Theory of Wing Sections, Abbott / v. DoenhoffCheersClaus Share this post Link to post Share on other sites
Mr. Konrad Lorentz 2 Report post Posted July 21, 2016 The theroy is introduced on page 111 - Chapter 6 - Families of Wing Sections The camber definition is on page 402 Maybe you needa profilea intersectioncurve for the camber offseta generic curve to combine both Share this post Link to post Share on other sites
Mr. KANG HAN 0 Report post Posted December 25, 2019 Hey guys: Any one has the info of naca66 a=0.8 mean camer line? On many occasions, I have run into this type of curve. As we know, many types of naca66 are included in CAESES, just don't know which one is "naca66 a=0.8 mean camer line" naca66.jpg Best Regards,ChenHey guy,Have you found a good way to establish the naca66 a=0.8 frofile? Share this post Link to post Share on other sites
