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A circular combustor configuration with multiple injection ports for mixing enhancementA circular combustor design by Ghorashi (1988) which resembles a continuously-stirred tank reactor with multiple injection ports is presented with a view to the enhanced control of mixing, NO(x) reduction, and combustion efficiency maximization. Attention is given to the prototype apparatus for this type of circular combustor, which takes the form of a transparent cold-flow reactor for flow visualization studies under 'chemically frozen' conditions.
Document ID
19900028334
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ghorashi, B. (NASA Lewis Research Center Cleveland, OH, United States)
Chun, K. (NASA Lewis Research Center Cleveland, OH, United States)
Kang, P. (NASA Lewis Research Center Cleveland, OH, United States)
Neidzwecki, R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Fluid Mechanics And Heat Transfer
Meeting Information
Meeting: Heat Transfer and Fluid Mechanics Institute Meeting
Location: Sacramento, Ca
Country: United States
Start Date: June 1, 1989
End Date: June 2, 1989
Accession Number
90A15389
Distribution Limits
Public
Copyright
Other

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