Email this article Aerodynamic Characteristics of Thin Cylindrical and Conical Shells in the Incompressible Flow
- Authors: Kalugin V.T.1, Lutsenko A.Y.1, Nazarova D.K.1
-
Affiliations:
- Bauman Moscow State Technical University
- Issue: Vol 61, No 3 (2018)
- Pages: 404-411
- Section: Aero- and Gas-Dynamics of Flight Vehicles and Their Engines
- URL: https://journal-vniispk.ru/1068-7998/article/view/230612
- DOI: https://doi.org/10.3103/S1068799818030133
- ID: 230612
Cite item
Open Access
Access granted
Subscription Access
Abstract
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.
About the authors
V. T. Kalugin
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
A. Yu. Lutsenko
Bauman Moscow State Technical University
Email: dknazarova@mail.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
D. K. Nazarova
Bauman Moscow State Technical University
Author for correspondence.
Email: dknazarova@mail.ru
Russian Federation, ul. 2ya Baumanskaya 5, str. 1, Moscow, 105005
Supplementary files
