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Engines and propellers for powered gliders and light airplanes (1938)

NASA Technical Reports Server (NTRS) · leaf 12

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N.A.C.A. Technical Memorandum No. 850 Jigs. 3,4,5 … S ^ 90 Figure 3.- Average curve showing u J u «S - 70 the relation between the engine output ani forward velocity at the condition of max-S Jh gQ imum rate of climb of powered ° io 40 50 30 20 gliders and light airplanes. *hp. Figure 5.- Weight per liter of light air- plane enelnes ae function of…

NASA Technical Reports Server (NTRS)

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