Engines and propellers for powered gliders and light airplanes (1938)
NASA Technical Reports Server (NTRS) · leaf 13
H.A.C.A. Technical Memorandum No. 850 Jigs. 6,7 10 6 ^ff,. kg/cm* 2 .2 .4 .6 .8 1.0 1.2 Displacement volume/cylinder, 1 Figure 6.- Mean effective pressure at maximum output as a function of cylinder displacement. … 0 1 2 3 4 5 6X1000 Rotational speed, r.p.m. ffigure 7.- Cylinder displacement, weight, and power supplied to propeller shaft for engines with a useful pro- peller output of 20 hp. as a function of the rotational speed.
NASA Technical Reports Server (NTRS)
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