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Effect of ambient temperature and humidity on emissions of an idling gas turbineThe effects of inlet pressure, temperature, and humidity on the oxides of nitrogen produced by an engine operating at takeoff power setting were investigated and numerous correction factors were formulated. The effect of ambient relative humidity on gas turbine idle emissions was ascertained. Experimentally, a nonvitiating combustor rig was employed to simulate changing combustor inlet conditions as generated by changing ambient conditions. Emissions measurements were made at the combustor exit. For carbon monoxide, a reaction kinetic scheme was applied within each zone of the combustor where initial species concentrations reflected not only local combustor characteristics but also changing ambient conditions.
Document ID
19780003137
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kauffman, C. W.
(Cincinnati Univ. OH, United States)
Date Acquired
August 9, 2013
Publication Date
October 1, 1977
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Eng. Emissions
Subject Category
Aircraft Propulsion And Power
Accession Number
78N11080
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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