FUEL HYDROGEN CONTENT AS AN INDICATOR OF RADIATIVE HEAT TRANSFER IN AN AIRCRAFT GAS TURBINE COMBUSTOR.

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Jackson, T.A.
Blazowski, W.S.
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Technical Report AFAPL-TR - Air Force Aero Propulsion Laboratory (United States) | 1979年 / 79-2014期
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摘要：
Eleven fuels representing a wide range of hydrogen content were studied using a T56 single can combustor rig. Fuel mixtures with hydrogen contents ranging from 9. 9 to 15. 9 per cent by weight were examined. The combustor inlet conditions simulated the discharge from both low and high pressure ratio gas turbine compressors operating at the cruise condition. Thermocouple data from the T56 liner were correlated with fuel hydrogen content using a new, nondimensional combuster liner.
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