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The Effect of Compressibility on Eight Full-Scale Propellers Operating in the Take-Off and Climbing Range (1938)
NASA Technical Reports Server (NTRS) · leaf 19
16 REPORT NO. 639—NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS … Figure 44—Propeller 4877; A/6=0.06. Figure 45—Propeller 4878; A/6=0.08. Figure 46.—Propeller 4879; /»/6=0.10. Figures 44, 45, and 46.—Effect of compressibility on propeller characteristics. Propeller diameters, 9)4 ft.; set 20° at 0.75/?; liquid-cooled engine nacelle. 1.2 1.0 .8 1.0 1.0 Climbing…NASA Technical Reports Server (NTRS)
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