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Aerodynamic principles of the direct lifting propeller (1934)
NASA Technical Reports Server (NTRS) · leaf 69
1T.A.C.A. Technical Memorandum Ho. 733 Figs. 17,18 2.0 1.5 a, cm0 (A = 6) b, Cjjjq (rotating wing) c, ca(a) (measurement) 1.0 d, c = 2.35 a lifting vortex. a .5 0 10 40 20 30 50 <x° 0 .10 .15 .05 . 20 .25 emo 3?iguro 17.-Comparison between circular wing and rectangular wing of equal profile (Clark… … Figure 18.-Induced inclination of the plane "substitute11 flow at the locus of tlio lifting propeller.NASA Technical Reports Server (NTRS)
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