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Fuel investigation in a tubular-type combustor of a turbojet engine
A series of 11 fuels ranging in volatility and including various types of hydrocarbons were tested in a single tubular combustion chamber of a turbojet engine under inlet-air conditions simulating engine operation at two speeds at an altitude of 40,000 feet. Temperature-rise data at various fuel-air ratios were obtained for each set of air-flow conditions. Results regarding the effect of combustor inlet-air conditions on temperature rise, four different series of tests, and a review of some general considerations are provided.
Date:
August 1, 1947
Creator:
Tischler, Adelbert O. & Dittrich, Ralph T.
System:
The UNT Digital Library