Interaction Between Parallel Streams of Subsonic and Supersonic Velocities
Author:
Affiliation:
1. Massachusetts Institute of Technology,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.11849
Reference9 articles.
1. The Interaction Between Boundary Layer and Shock Waves in Transonic Flow
Cited by 34 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. Oblique radiative shocks, including their interactions with nonradiative polytropic shocks;Physics of Plasmas;2011-05
2. Preface;Asymptotic Theory of Supersonic Viscous Gas Flows;2008
3. 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
4. On upstream influence in supersonic flows;Journal of Fluid Mechanics;2005-09-05
5. On Disturbance Propagation in Internal-Flow Boundary Layers;Fluid Dynamics;2004-07
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