The knocking characteristics of fuels in relation to maximum permissible performance of aircraft engines (1939)
NASA Technical Reports Server (NTRS) · leaf 6
t the leaded fuel should be capable of engines of larger bore, the data for which are given in operation at a compression ratio of about 12, provided tables II to V, the effect of the increased temperature that the inlet-air temperature does not exceed 120° F. caused by increasing the compression… … 320 160 200 240 280 IZO Inlet-air temperature, °F. Fiocbe 5.—Effect of Inlet-air temperature on maximum permissible density factor ISO 200 240 280 120 for a series of fuel blends. Pent-roof combustion chamber; engine speed, 2,500 Inlet- air temperature, *F. r. p. m.; fuel-air ratio, 0.078;…
NASA Technical Reports Server (NTRS)
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