Flow past Rankine’s Half-Body of Revolution

G. L. Korolev; Королев Г. Л.; Vik. V. Sychev; Сычёв Вик. В.

doi:10.31857/S0568528122600576

Flow past Rankine’s Half-Body of Revolution

作者: Korolev G.L.¹, Sychev V.V.¹
隶属关系:
1. Central Aerohydrodynamic Institute (TsAGI)
期: 编号 2 (2023)
页面: 85-89
栏目: Articles
URL: https://vietnamjournal.ru/1024-7084/article/view/672458
DOI: https://doi.org/10.31857/S0568528122600576
EDN: https://elibrary.ru/NSYFUF
ID: 672458

如何引用文章

全文:

开放存取

##reader.subscriptionAccessGranted##
受限制的访问

订阅存取

详细
作者简介
参考
补充文件
统计

详细

An axisymmetric incompressible flow past Rankine’s half-body of revolution is investigated at high Reynolds numbers. It is established that the solution of the problem for the system of boundary layer equations does not involve the line of zero surface friction. The low under consideration is separationless, which is in complete agreement with the available experimental data.

关键词

Rankine solution, boundary layer, separation

作者简介

G. Korolev

Central Aerohydrodynamic Institute (TsAGI)

Email: glk777@mail.ru
Zhukovsky, Moscow oblast, 140180 Russia

Vik. Sychev

Central Aerohydrodynamic Institute (TsAGI)

编辑信件的主要联系方式.
Email: glk777@mail.ru
Zhukovsky, Moscow oblast, 140180 Russia

参考

Van Dyke M.D. Second-order slender-body theory − axisymmetric flow // NASA Tech. Rep. 1959. R-47. 26 p.
Cole J.D. Perturbation methods in applied mathematics. Waltham: Blaisdell, 1968. 260 p.
Jones R.T. Leading-edge singularities in thin-airfoil theory // J. Aeronaut. Sci. 1950. V. 17. № 5. P. 307−310.
Van Dyke M.D. Second-order subsonic airfoil theory including edge effects // NACA Rep. 1956. № 1274. 23 p.
Van Dyke M. Perturbation methods in fluid mechanics. Stanford: Parabolic Press, 1975. 271 p.
Rankine W.J.M. On the mathematical theory of stream-lines, especially those with four foci and upwards // Phil. Trans. Roy. Soc. London. 1871. V. 161. Pt. II. P. 267–306.
Сычев В.В., Башкин В.А. Лекции по теоретической гидродинамике. Ч. I. Учебное пособие. М.: МФТИ, 2003. 188 с.
Rosenhead L. (Ed.) Laminar boundary layers. Oxford: Clarendon Press, 1963, 688 p.
Homann F. Der Einfluβ groβer Zähigkeit bei der Strömung um den Zylinder und um die Kugel // ZAMM. 1936. Bd. 16. H. 3. S. 153−164.
Королев Г.Л., Сычев Вик. В. О пограничном слое при обтекании полутела Рэнкина // Изв. РАН. МЖГ. 2021. № 6. С. 62–65.
Werlé H. Le décollement sur les corps de révolution à basse vitesse // La Rech. Aéron. 1962. № 90. P. 3−14.
Van Dyke M. An album of fluid motion. Stanford: Parabolic Press, 1982. 176 p.