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Application of Cebeci’s method for solving time-dependent problems of the incompressible boundary layer
- Authors: Kharitonova A.N.1, Shakhov V.G.2
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Affiliations:
- State Research and Production Space Rocket Center “TsSKB – Progress”, Samara
- Samara State Aerospace University
- Issue: Vol 10, No 2 (2011)
- Pages: 106-111
- Section: AIRCRAFT AND SPACE ROCKET ENGINEERING
- URL: https://journals.ssau.ru/vestnik/article/view/1671
- DOI: https://doi.org/10.18287/2541-7533-2011-0-2(26)-106-111
- ID: 1671
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Abstract
The opportunity of using the Cebeci method to solve time-dependent problems of the incompressible boundary layer is dealt with in the paper. The method helped to solve the problems of analyzing the boundary layer on a flat plate streamlined in the longitudinal direction; the flow around a circular cylinder in the transverse direction; the longitudinal flow of the NACA 0012 airfoil for the zero angle of attack; the flow around a moving circular cylinder for the case of laminar non-stationary boundary layer.
About the authors
A. N. Kharitonova
State Research and Production Space Rocket Center “TsSKB – Progress”, Samara
Author for correspondence.
Email: annqwer@mail.ru
Head of Group
Russian FederationV. G. Shakhov
Samara State Aerospace University
Email: shakhov@ssau.ru
Candidate of Technical Sciences
Professor
Head of Aerohydrodynamic Department
Russian FederationReferences
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- Шлихтинг, Г. Теория пограничного слоя [Текст] / Г. Шлихтинг. – М.: Наука, 1974. – 712 с.
- Cebeci, T. Computational fluid dynamics for engineers [Текст] / T. Cebeci, J. P. Shao, F. Kafyeke, E. Laurendeau. – California: Horizons Publishing Inc., 2005. – 396 с.
- Лойцянский, Л. Г. Ламинарный пограничный слой [Текст] / Л. Г. Лойцянский. – М.: Государственное издательство физико-математической литературы, 1962. – 478 с.
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