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Engine Operation in Flight for Minimum Fuel Consumption (1939)

NASA Technical Reports Server (NTRS) · leaf 17

An illustration from Engine Operation in Flight for Minimum Fuel Consumption, 1939, leaf 17
Manifold pressure, in. Hg abs. manifold pressure at two engine speeds. (a) Fuel-air ratio, optimum, (b) Fuel-air ratio,O.lQ^" C.F*R. engine; 86-oetane fuel; constant Figure 6.- Effect of manifold pressure, engine m spark advance. speed, and fuel-air ratio on rate of fuel consumption at sea level*…

NASA Technical Reports Server (NTRS)

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