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 Figure 6.- Pressure distribu- tion chenge of original profile. Figure 7.- Prohibited ■ores sure distribution change. Figure 8.- Course '03 of 1 - velocity and potential along the development of the…
NASA Technical Reports Server (NTRS)
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