Modification of wing-section shape to assure a predetermined change in pressure distribution (1935)
NASA Technical Reports Server (NTRS) · leaf 19
N.A.C.A. Technical Memorandum Ho 767 Pigs. 5,6,7,8,9 Figure 5. Original airfoil Modified profile … 360° Figure 9.- Course of E(v]A l/v) and j(v]£ l/v) along the circle periphery in plane z.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
