Method for the determination of the spanwise lift distribution (1935)
NASA Technical Reports Server (NTRS) · leaf 54
Figs. 9,10,11,12,13 N.A.O.A. Teobnical Memorandum No. 778 … tell as Flight condition ca total - +1.0 0 0,50 4*> -&3 Figure 12.- Elliptical zero distri- bution and corresponding Figure 13.- Results of lift distribution twist as used in the ex- in first and fourth approach. ample.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
