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Engine performance with a hydrogenated safety fuel (1933)

NASA Technical Reports Server (NTRS) · leaf 13

An illustration from Engine performance with a hydrogenated safety fuel, 1933, leaf 13
S3 & O P, l-» ft Izj o * O 1500 r.p.m. S <D X 1800 r.p.m. A 1200 r.p.m. … Fuel quantity, lb./cycle Figure 5.~h.m.e.p. and fuel consumption at speeds of 1200, 1500, and 1800 r.p.m. and at a compression ratio of 5.5 with atmospheric inlet pressure, -using safety fuel and a valve overlap of 112 . 2 0*1 ■ I

NASA Technical Reports Server (NTRS)

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