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Ignition/combustion processesThe overall objectives for this initial technology are to generate an advanced, comprehensive combustion analytical code, and to verify the combustion flow dynamic predictions from this model with hot test experimental data.
Document ID
19850018598
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Pryor, D. E.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 12, 2013
Publication Date
April 1, 1985
Publication Information
Publication: Advan. High Pressure O2(H2 Technol.
Subject Category
Inorganic And Physical Chemistry
Accession Number
85N26909
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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