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- W1985111227 abstract "The performance of an advanced small high temperature rise combustor was experimentally determined at NASA-Lewis. The combustor was designed to meet the requirements of advanced high temperature, high pressure ratio turboshaft engines. The combustor featured an advanced fuel injector and an advanced segmented liner design. The full size combustor was evaluated at power conditions ranging from idle to maximum power. The effect of broad fuel properties was studied by evaluating the combustor with three different fuels. The fuels used were JP-5, a blend of Diesel Fuel Marine/Home Heating Oil, and a blend of Suntec C/Home Heating Oil. The fuel properties effect on the performance of the combustion in terms of pattern factor, liner temperatures, and exhaust emissions are documented." @default.
- W1985111227 created "2016-06-24" @default.
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- W1985111227 creator A5036036491 @default.
- W1985111227 date "1989-07-12" @default.
- W1985111227 modified "2023-09-27" @default.
- W1985111227 title "Fuel properties effect on the performance of a small high temperature rise combustor" @default.
- W1985111227 cites W1989276004 @default.
- W1985111227 doi "https://doi.org/10.2514/6.1989-2901" @default.
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