Comparison of wall mixing concepts for scramjet combustors
Author:
Affiliation:
1. Virginia Polytechnic Inst. and State Univ., Blacksburg
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1994-587
Reference20 articles.
1. I . Mays, R. B., Thomas, R. H., and Schetz, J. A, "Low angle Injection into a Supersonic Flow," AIAA89-2461
2. Cutler, A. D., and Levey, B. S. "Vortex Breakdown in asupersonic Jet,"AIAA-91-1815, 1991.
3. Kraus, D.K., and Cutler, A. D. "Mixing Enhancement by the Use of SwirlingJets," AIAA-93-3126.
4. Noncircular jet dynamics in supersonic combustion
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