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Parametric test results of a swirl-can combustor.Pollutant levels of oxides of nitrogen, unburned hydrocarbons, and carbon monoxide were measured for three models of an experimental, annular swirl can combustor. The combustor was 1.067 meters in outer diameter, incorporated 120 modules, and was specifically designed for elevated exit temperature performance. Test conditions included combustor inlet temperatures of 589, 756, and 839 K, inlet pressures of 3 to 6.4 atmospheres, reference velocities of 21 to 38 meters per second, and combustor equivalence ratios, based on total combustor flows, of 0.206 to 1.028. Maximum oxides of nitrogen emission index values occurred at an equivalence ratio of 0.7 with lower values measured for both higher and lower equivalence ratios.
Document ID
19730050669
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Niedzwiecki, R. W.
Jones, R. E.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 7, 2013
Publication Date
June 1, 1973
Subject Category
Propulsion Systems
Meeting Information
Meeting: National Meeting
Location: Detroit, MI
Start Date: June 4, 1973
End Date: June 6, 1973
Sponsors: American Institute of Chemical Engineers
Accession Number
73A35471
Distribution Limits
Public
Copyright
Other

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