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Engine Operation in Flight for Minimum Fuel Consumption (1939)
NASA Technical Reports Server (NTRS) · leaf 21
Manifold pressure, in* abs. (a) Fuel-air ratio, optimum* ^ (a) Fuel tanks empty* (b) " 11 " 0.10. (b) 11 " full. Figure 10.- Effect of manifold pressure, engine « Figure 9 *- Flight mileage for conditions of figures speed, and fuel-air ratio on rate of ^ 5 and 7 (sea level). fuel consumption at…NASA Technical Reports Server (NTRS)
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