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A detailed numerical model of a supersonic reacting mixing layerA current research effort is underway at the NASA Langley Research Center to achieve a detailed understanding of important phenomena present when a supersonic flow undergoes chemical reaction. A computer program has been developed to study the details of such flows. The program has been constructed to consider the multicomponent diffusion and convection of important species, the finite-rate reaction of these species, and the resulting interaction between the fluid mechanics and chemistry. Code results from the analysis of a spatially developing and reacting mixing layer are presented, and conclusions are drawn regarding the structure of the evolving layer and its associated flame.
Document ID
19860057898
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Drummond, J. P.
(NASA Langley Research Center Hampton, VA, United States)
Rogers, R. C.
(NASA Langley Research Center Hampton, VA, United States)
Hussaini, M. Y.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 86-1427
Accession Number
86A42636
Distribution Limits
Public
Copyright
Other

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