Compression-ignition engine performance at altitudes and at various air pressures and temperatures
Description:
From Summary: "Engine test results are presented for simulated altitude conditions. A displaced-piston combustion chamber on a 5- by 7-inch single cylinder compression-ignition engine operating at 2,000 r.p.m. was used. Inlet air temperature equivalent to standard altitudes up to 14,000 feet were obtained. Comparison between performance at altitude of the unsupercharged compression-ignition engine compared favorably with the carburetor engine."
Date:
November 1937
Creator:
Moore, Charles S. & Collins, John H., Jr.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department