Numerical study of supersonic combustion using a finite rate chemistry model
Author:
Affiliation:
1. Old Dominion University, Norfolk, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-309
Reference17 articles.
1. Using a global hydrogen-air combustion model in turbulent reacting flow calculations
Cited by 7 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Effects of tandem injection on compressible turbulent shear layer;8th AIAA International Space Planes and Hypersonic Systems and Technologies Conference;1998-04-27
2. On the characteristics of turbulent multiple jets diffusion flame. I - Cold flow;32nd Thermophysics Conference;1997-06-23
3. Computation of nonequilibrium hypersonic viscous flow about a Martian Entry Vehicle (MEV);32nd Aerospace Sciences Meeting and Exhibit;1994-01-10
4. Thermochemical nonequilibrium and radiative interactions in supersonic hydrogen-air combustion;30th Aerospace Sciences Meeting and Exhibit;1992-01-06
5. Investigation of radiative interactions in chemically reacting supersonic internal flows;29th Aerospace Sciences Meeting;1991-01-07
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