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The effects of detailed chemistry and transport on microgravity droplet combustionA brief overview of recent advances in the theoretical study of microgravity droplet combustion is presented. Much of this work has centered on the development and utilization of sphero-symmetric transient numerical models which consider detailed gas phase chemistry and transport as well as energy and/or species transport within a regressing condensed phase. Numerical results for microgravity combustion and vaporization of methanol, methanol/water, heptane, and heptane/hexadecane droplets are summarized along with refinements in chemical kinetics and the development of a new two-dimensional axi-symmetric model.
Document ID
19960008395
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Marchese, A. J.
(Princeton Univ. NJ, United States)
Lee, J. C.
(Princeton Univ. NJ, United States)
Held, T. J.
(Princeton Univ. NJ, United States)
Dryer, F. L.
(Princeton Univ. NJ, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Publication Information
Publication: NASA. Lewis Research Center, The 3rd International Microgravity Combustion Workshop
Subject Category
Materials Processing
Accession Number
96N15561
Funding Number(s)
CONTRACT_GRANT: DE-F604-90AL-65460
CONTRACT_GRANT: NAG3-1231
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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