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Computational Modeling of the Structure and Extinction of Flame Balls in a Microgravity EnvironmentCombustion models that simulate pollutant formation and study chemically controlled extinction limits in flames often combine detailed chemical kinetics with complicated transport phenomena. One of the simplest models in which these processes are studied is the plane premixed laminar flame. This problem is appealing due to its simple flow geometry and it has been used by kineticists in understanding elementary reaction mechanisms in the oxidation of fuels. Although premixed flames have been studied extensively (experimentally and numerically) in a normal Earth based gravity environment, there is relatively little experimental and virtually no numerical investigations of these systems in a microgravity environment. To this end, we have begun a program designed to study computationally the effects of radiation losses on spherically symmetric premixed hydrogen-air flames in a microgravity environment in which there are no convective flows. We are considering a detailed transport and finite rate multistep kinetics model. To be able to compute solutions (both stable and unstable) in the neighborhood of the lean and rich extinction limits, we must modify the basic solution algorithm to include an arclength continuation procedure. In this way a parameter such as the equivalence ratio can be varied while still having a computationally stable algorithm.
Document ID
19970020605
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
M D Smooke
(Yale University New Haven, 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
97N21878
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
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