Performance of Several Combustion Chambers Designed for Aircraft Oil Engines (1928)
NASA Technical Reports Server (NTRS) · leaf 6
5 PERFORMANCE OF COMBUSTION CHAMBERS … Fig. 1.—Arrangement of Liberty type test engine and apparatus INJECTION SYSTEM The fuel-injection systems for the tests reported on cylinder heads designated as Nos. 1 and 3 comprised a primary gear pump supplying oil at 90 pounds per square inch pressure to a cam- actuated impact-type injection…
NASA Technical Reports Server (NTRS)
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