Effect of fuel on performance of a single combustor of an I-16 turbojet engine at simulated altitude conditions
Description:
As part of a study of the effects of fuel composition on the combustor performance of a turbojet engine, an investigation was made in a single I-16 combustor with the standard I-16 injection nozzle, supplied by the engine manufacturer, at simulated altitude conditions. The 10 fuels investigated included hydrocarbons of the paraffin olefin, naphthene, and aromatic classes having a boiling range from 113 degrees to 655 degrees F. They were hot-acid octane, diisobutylene, methylcyclohexane, benzen…
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Date:
July 3, 1947
Creator:
Zettle, Eugene V.; Bolz, Ray E. & Dittrich, R. T.
Item Type:
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Partner:
UNT Libraries Government Documents Department