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Application of a two-dimensional parabolic computer program to prediction of turbulent reacting flowsThe capabilities of a computer program are explored, and computed results are compared with data. The comparisons are restricted to two-dimensional flows. Subsonic and supersonic flows, ducted and nonducted, reacting and nonreacting, are considered. An evaluation of models used for turbulence and chemical reaction was included. Constants in the dissipation rate of turbulent kinetic energy, turbulence model, which produces mixing in good agreement with data, are the same for all calculations. Experimental data are reported for coaxial injection at matched pressure (1 atm or 101.3 kPa) of a cold, Mach 2, hydrogen jet into a hot, Mach 2, vitiated airstream. Profiles of pitot pressure and gas composition obtained from water cooled probes are reported and compared with theoretical results.
Document ID
19780012520
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Evans, J. S.
(NASA Langley Research Center Hampton, VA, United States)
Schexnayder, C. J., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Beach, H. L., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1978
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TP-1169
Accession Number
78N20463
Funding Number(s)
PROJECT: RTOP 505-05-43-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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