Axisymmetric Viscous Flow Past Very Slender Bodies of Revolution

Author:

YASUHARA M.1

Affiliation:

1. Nagoya University,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Cited by 41 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. 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

2. Unsteady hypersonic boundary layers for slender axisymmetric bodies with large injection rates;International Journal of Engineering Science;1992-06

3. Semi-similar solution of an unsteady compressible three-dimensional stagnation point boundary layer flow with massive blowing;International Journal of Engineering Science;1985-01

4. Transverse Curvature Effects on a Slender Cone with Heat Transfer and Angle of Attack;ZAMM - Zeitschrift für Angewandte Mathematik und Mechanik;1983

5. Compressible boundary-layer flow at a three-dimensional stagnation point with massive blowing;International Journal of Heat and Mass Transfer;1982-11

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