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Mixing of Pure Air Jets with a Reacting Fuel-Rich CrossflowJets in a crossflow play an integral role in practical combustion systems such as can and annular gas turbine combustors in conventional systems, and the Rich-burn/Quick-mix/Lean-burn (RQL) combustor utilized in stationary applications and proposed for advanced subsonic and supersonic transports. The success of the RQL combustor rests with the performance of the quick-mixing section that bridges the rich and lean zones. The mixing of jet air with a rich crossflow to bring the reaction to completion in the lean zone must be performed rapidly and thoroughly in order to decrease the extent of near-stoichiometric fluid pocket formation. Fluid pockets at near-stoichiometric equivalence ratios are undesirable because the high temperatures attained accelerate pollutant formation kinetics associated with nitric oxide (NO). The present study develops a model experiment designed to reveal the processes that occur when jet air is introduced into hot effluent emanating from a fuel-rich reaction zone.
Document ID
19970017837
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Leong, M. Y.
(California Univ. Irvine, CA United States)
Samuelsen, G. S.
(California Univ. Irvine, CA United States)
Holdeman, J. D.
(NASA Lewis Research Center Cleveland, OH United States)
Date Acquired
September 6, 2013
Publication Date
April 1, 1997
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA-TM-107430
NAS 1.15:107430
WCC/CI Paper 97S-034
E-10684
Meeting Information
Meeting: Western States Section
Location: Livermore, CA
Country: United States
Start Date: April 14, 1997
End Date: April 17, 1997
Sponsors: Combustion Inst.
Accession Number
97N19949
Funding Number(s)
PROJECT: RTOP 537-02-20
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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