The Interaction of Shock Waves with Boundary Layers on a Flat Surface
Author:
Affiliation:
1. Massachusetts Institute of Technology,
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Link
http://arc.aiaa.org/doi/pdf/10.2514/8.1916
Reference37 articles.
1. Some Experiments on the Interaction of Shock Waves With Boundary Layers on a Flat Plate
Cited by 30 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. Survey of control techniques to alleviate repercussions of shock-wave and boundary-layer interactions;Advances in Aerodynamics;2022-08-18
2. Shock Wave and Boundary Layer Interactions;Theoretical and Experimental Aerodynamics;2018-12-16
3. Highly cited literature of high-speed compressible flow research;Aerospace Science and Technology;2013-04
4. Preface;Asymptotic Theory of Supersonic Viscous Gas Flows;2008
5. 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
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