Surface mass injection at supersonic and hypersonic speeds as a problem in turbulent mixing. II - Axially-symmetric flow
Author:
Affiliation:
1. California Institute of Technology, Pasadena, Calif.
2. TRW Systems, Redondo Beach, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6329
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1. Blowing from a porous cone with an embedded shock wave
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Cited by 12 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. Continuum-plasma solution surrounding nonemitting spherical bodies;Physics of Plasmas;2009-06
2. Bibliography**References to the books by Russian and other non-English-speaking authors are given in accordance with their English translations, if there are any and they are known to the authors or the translator. As for the papers from Russian scientific journals cited in this book, most of them were published in the following three journals: Prikladnaya Matematika i Mekhanika, Izvestiya Akademii Nauk, ser. Mekhanika Zhidkosti i Gaza, and Zhurnal Prikladnoi Meknaniki i Tekhnicheskoi Fiziki. All the three journals are translated into English – the first by Elsevier under the name Applied Mathematics and Mechanics and the other two by Springer as Fluid Dynamics and Journal of Applied Mechanics and Technical Physics. References to the papers published in these journals are given in accordance with the above translations, while references to the papers from other Russian journals in accordance with the original publications.;Asymptotic Theory of Supersonic Viscous Gas Flows;2008
3. Skin Friction Prediction for High-Speed Turbulent Boundary Layers with Ablation;Journal of Spacecraft and Rockets;2004-09
4. Lester Lees and Hypersonic Aerodynamics;Journal of Spacecraft and Rockets;2003-07
5. Skin Friction Prediction for High-Speed Turbulent Boundary Layers with Ablation;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
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