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Dynamics and Structure of Weakly-Strained Flames at Normal and MicrogravityStrained laminar flames have been the subject of extensive studies the last thirty years or so, typically in opposed-jet, stagnation-flow configurations. The motivation behind such extensive efforts emerges from the relevance of such flames to a number of combustion phenomena and issues. First, it is believed that such flames are of relevance to turbulent combustion, given that under certain conditions, turbulent flames can be viewed as an assembly of strained laminar flamelets. Second, the opposed-jet, stagnation-flow configuration is a particularly meritorious configuration, in which the details of the physico-chemical processes can be probed and understood. More specifically, the stagnation-flow configuration allows for the accurate determination of fundamental flame properties and can be modeled conveniently with the use of detailed description of chemical kinetics and molecular transport. Thus, on one hand the interaction between fluid mechanics and chemical kinetics can be investigated from first principles and on the other, existing kinetic and/or transport models can be (partially) validated with confidence. The response and phenomena of interest of laminar flames are quite different, depending on whether the strain rate is low or high.
Document ID
19970020603
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Christine M Vagelopoulos
(University of Southern California Los Angeles, United States)
Fokion N Egolfopoulos
(University of Southern California Los Angeles, United States)
Fletcher J Miller
(Case Western Reserve University Cleveland, United States)
Date Acquired
August 17, 2013
Publication Date
May 1, 1997
Publication Information
Publication: Fourth International Microgravity Combustion Workshop
Publisher: National Aeronautics and Space Administration
Subject Category
Materials Processing
Report/Patent Number
NASA-CP-10194
Meeting Information
Meeting: Fourth International Microgravity Combustion Workshop
Location: Cleveland, OH
Country: US
Start Date: May 19, 1997
End Date: May 21, 1997
Sponsors: National Aeronautics and Space Administration
Accession Number
97N21876
Funding Number(s)
CONTRACT_GRANT: NAG3-1615
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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