Мақаланы E-mail арқылы жіберу Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
- Авторлар: Kalugin V.T.1, Lutsenko A.Y.1, Nazarova D.K.1
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Мекемелер:
- Bauman Moscow State Technical University
- Шығарылым: Том 61, № 3 (2018)
- Беттер: 404-411
- Бөлім: 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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Аннотация
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.
Авторлар туралы
V. Kalugin
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Ресей, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
A. Lutsenko
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Ресей, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
D. Nazarova
Bauman Moscow State Technical University
Хат алмасуға жауапты Автор.
Email: dknazarova@mail.ru
Ресей, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
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