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NASA-Chinese Aeronautical Establishment (CAE) SymposiumSeveral topics relative to combustion research are discussed. A numerical study of combustion processes in afterburners; the modeling of turbulent, reactive flow; gas turbine research; modeling of dilution jet flow fields; and chemical shock tubes as tools for studying high-temperature chemical kinetics are among the topics covered.
Document ID
19870010834
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Date Acquired
September 5, 2013
Publication Date
January 1, 1986
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.55:2433
E-3033
NASA-CP-2433
Report Number: NAS 1.55:2433
Report Number: E-3033
Report Number: NASA-CP-2433
Accession Number
87N20267
Funding Number(s)
PROJECT: RTOP 505-62-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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