Cooling Characteristics of a 2-Row Radial Engine (1937)
NASA Technical Reports Server (NTRS) · leaf 7
general operation and power output of 24, and 20 inches of mercury absolute and at an air the engine. The maximum rate was with the mixture speed of 116 miles per hour. For each of these runs control set full rich. the desired engine speed was obtained at each air- The difference in cylinder… … Figure 3.—The X04U-2 airplane mounted in the full-scale tunnel ready for test. The effect of engine speed on the cylinder tempera- 2,100 r. p. m. and at air speeds of 85 and 120 miles per tures for a constant brake horsepower and a constant hour, respectively. air speed of 119 miles per hour was…
NASA Technical Reports Server (NTRS)
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