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The comparative performance of an aviation engine at normal and high inlet air temperatures (1928)

NASA Technical Reports Server (NTRS) · leaf 16

An illustration from The comparative performance of an aviation engine at normal and high inlet air temperatures, 1928, leaf 16
VE PESFOEIIAITGE OF A:n AVIATION ENGINE Data for tke Liberty engine, giving the average depressions in two manifolds below th.e existing carburetor pressure, are shown on Figures 12 and 13, and for the Wright engiae, on Figure 14. From the average of the many observations taken, it was found that a… … Revolufions per mhufe Revolufions per minufs RevoluNans per minufe Fig. 12.—Liberty 12 engine. Depressions in manifold belovr existing pressure at entrance to carburetor for various air temperatures (avera£e of front rigbt and rear left manifolds) 3.S 2.0 O '3o4,bsnza/anc/ I r 70 7. gaso/ihe,…

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