Comparison of Three Radiative Formulations for Interactions in Three-Dimensional Boundary Layers
Author:
Affiliation:
1. Tuskegee Institute, Tuskegee, Alabama
2. Vachon, Nix, & Associates, Atlanta, Georgia
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.48554
Reference19 articles.
1. Johnson, R. E. "Radiation Shape Factor and Loading Analysis on a Hypersonic Vehicle in the Vicinity of a Nuclear Blast," M.S. Thesis,Auburn University, Auburn, Ala. March 1977.
2. 5Adams Jr., J. C. "Analysis of the Three-Dimensional Compressible Turbulent Boundary Layer on a Sharp Cone at Incidence in Supersonic and Hypersonic Flow," Arnold Engineering Development Center, Arnold AirForce Station, Tenn., AEDC-TR-72-66,June 1972
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1. Non-grey radiation in a liquid rocket combustion chamber;26th Joint Propulsion Conference;1990-07-16
2. Swept shock/boundary-layer interactions - Tutorial and update;28th Aerospace Sciences Meeting;1990-01-08
3. Interaction of radiation with turbulence - Application to a combustion system;Journal of Thermophysics and Heat Transfer;1987-01
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