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Radiation Effects on Flow Characteristics in Combustion ChambersA JANNAF sponsored workshop was held to discuss the importance and role of radiative heat transfer in rocket combustion chambers. The potential impact of radiative transfer on hardware design, reliability, and performance was discussed. The current state of radiative transfer prediction capability in CFD modeling was reviewed and concluded to be substantially lacking in both the physical models used and the radiative property data available. There is a clear need to begin to establish a data base for making radiation calculations in rocket combustion chambers. A natural starting point for this effort would be the NASA thermochemical equilibrium code (CEC).
Document ID
19910007819
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Brewster, M. Q.
(Illinois Univ. at Urbana-Champaign Urbana, IL, United States)
Gross, Klaus W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1989
Publication Information
Publication: JHU, The 26th JANNAF Combustion Meeting, Volume 2
Subject Category
Spacecraft Propulsion And Power
Meeting Information
Meeting: 26th JANNAF Combustion Meeting
Location: Pasadena, CA
Country: United States
Start Date: October 23, 1989
End Date: October 27, 1989
Sponsors: NASA Headquarters, Department of the Army, Department of the Air Force, Department of the Navy
Accession Number
91N17132
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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