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Effect of swirl on premixed combustionCombustion in a premixed swirl combustor composed of confined concentric jets (5 cm and 10 cm diameter) were studied. The inner flow is fuel and air; the outer flow is air. Both flows may contain swirl either in the same or opposite directions. The combustor operates at one atmosphere without preheat; methane and propane were used as fuels. Related analyses and experiments were also performed for water flows and isotherm air flows. In these studies, a number of important concepts regarding premixing/prevaporized, swirl stabilized combustion were developed. Some of the more significant are discussed.
Document ID
19790016839
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Gouldin, F. C.
(Cornell Univ. Ithaca, NY, United States)
Leibovich, S.
(Cornell Univ. Ithaca, NY, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Premixed Prevaporized Combustor Technol. Forum
Subject Category
Aircraft Propulsion And Power
Accession Number
79N25010
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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