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Aerothermal modeling program, phase 2. Element C: Fuel injector-air swirl characterizationThe main objectives of the NASA-sponsored Aerothermal Modeling Program, Phase 2--Element C, are experimental evaluation of the air swirler interaction with a fuel injector in a simulated combustor chamber, assessment of the current two-phase models, and verification of the improved spray evaporation/dispersion models. This experimental and numerical program consists of five major tasks. Brief descriptions of the five tasks are given.
Document ID
19890003521
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Mostafa, A. A. (General Motors Corp. Detroit, MI, United States)
Mongia, H. C. (General Motors Corp. Detroit, MI, United States)
Mcdonnell, V. G. (General Motors Corp. Detroit, MI, United States)
Samuelsen, G. S. (General Motors Corp. Detroit, MI, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1986
Publication Information
Publication: NASA, Lewis Research Center, Turbine Engine Hot Section Technology 1986
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
89N12892
Funding Number(s)
CONTRACT_GRANT: NAS3-24350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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