Modification of wing-section shape to assure a predetermined change in pressure distribution (1935)
NASA Technical Reports Server (NTRS) · leaf 20
U.A.C.A. Technical Memorandum ITo. 767 Pigs. 10,11,12,13,14,15,16 .05- .05 .05-}- ,05- l\ E E J 6.2 0 0^2 e i:o 0 -.05 -L -.05 -.05-- -.05-1- Figure 10. Figure 11. Figures 1C,11.-Course of E and J along the profile contour projected on axis I and on axis r\. .05 + .05- .05- E J J -0.1 -I h 1?0 V.… … Figures 14,15.-Course of R and J along axes l2and- 12* A1/1-0.5 A|,An Ati~n Figure 16.-The resultant 1.0 s 2.0 displacements A i and Ari of the profile points. -0.5
NASA Technical Reports Server (NTRS)
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