Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
- Autores: Kalugin V.T.1, Lutsenko A.Y.1, Nazarova D.K.1
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Afiliações:
- Bauman Moscow State Technical University
- Edição: Volume 61, Nº 3 (2018)
- Páginas: 404-411
- Seção: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journals.rcsi.science/1068-7998/article/view/230612
- DOI: https://doi.org/10.3103/S1068799818030133
- ID: 230612
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Resumo
The paper presents aerodynamic characteristics of thin cylindrical and conical shells in the incompressible flow. Experimental data and results of numerical simulation in the OpenFoam software are compared. It is shown that the aerodynamic characteristics of the thin shells differ from the aerodynamic characteristics of the corresponding solid bodies and depend on the shell geometry parameters.
Sobre autores
V. Kalugin
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Rússia, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
A. Lutsenko
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Rússia, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
D. Nazarova
Bauman Moscow State Technical University
Autor responsável pela correspondência
Email: dknazarova@mail.ru
Rússia, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
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