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Aerothermal modeling program, phase 2The main objectives of the Aerothermal Modeling Program, Phase 2 are: to develop an improved numerical scheme for incorporation in a 3-D combustor flow model; to conduct a benchmark quality experiment to study the interaction of a primary jet with a confined swirling crossflow and to assess current and advanced turbulence and scalar transport models; and to conduct experimental evaluation of the air swirler interaction with fuel injectors, assessments of current two-phase models, and verification the improved spray evaporation/dispersion models.
Document ID
19880001767
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mongia, H. C.
(Minnesota Univ. Minneapolis., United States)
Patankar, S. V.
(Purdue Univ. West Lafayette, IN., United States)
Murthy, S. N. B.
(Purdue Univ. West Lafayette, IN., United States)
Sullivan, J. P.
(General Motors Corp. Detroit, MI, United States)
Samuelsen, G. S.
(California Univ. Irvine., United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1985
Publication Information
Publication: NASA. Lewis Research Center, Turbine Engine Hot Section Technology, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
88N11149
Funding Number(s)
CONTRACT_GRANT: NAS3-24350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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