Abstract:
Results of experimental and numerical investigations of the flow around an elongated axisymmetric body of revolution in a low-velocity wind tunnel with a closed test section and in a free flow are reported. The Reynolds number based on the body length is varied in the interval from 2.75⋅106 to 9.40⋅106. The problem is solved numerically under the assumption of an axisymmetric steady incompressible flow with the use of the ANSYS Fluent software. It is demonstrated that the test section walls produce a significant effect on the flow character and aerodynamic performances of the body of revolution for the case where the blockage factor of the test section by the body of revolution is formally within 2%.
Keywords:
body of revolution, turbulent boundary layer, experiment, numerical simulation, flow properties.
This study was performed within the framework of the State Contract (State Registration Number 121030500158-0). The experiments were performed at the Collective Use Center “Mekhanika” (Mechanics)
based at the Khristianovich Institute of Theoretical and Applied Mechanics of the Siberian Branch of the Russian Academy of Sciences.
Citation:
V. I. Kornilov, A. N. Popkov, “Simulation of the flow around an axisymmetric body in the absence of free boundaries of the flow”, Prikl. Mekh. Tekh. Fiz., 64:2 (2023), 27–38; J. Appl. Mech. Tech. Phys., 64:2 (2023), 198–207
\Bibitem{KorPop23}
\by V.~I.~Kornilov, A.~N.~Popkov
\paper Simulation of the flow around an axisymmetric body in the absence of free boundaries of the flow
\jour Prikl. Mekh. Tekh. Fiz.
\yr 2023
\vol 64
\issue 2
\pages 27--38
\mathnet{http://mi.mathnet.ru/pmtf1253}
\crossref{https://doi.org/10.15372/PMTF202215114}
\elib{https://elibrary.ru/item.asp?id=50441312}
\transl
\jour J. Appl. Mech. Tech. Phys.
\yr 2023
\vol 64
\issue 2
\pages 198--207
\crossref{https://doi.org/10.1134/S0021894423020049}
Linking options:
https://www.mathnet.ru/eng/pmtf1253
https://www.mathnet.ru/eng/pmtf/v64/i2/p27
This publication is cited in the following 2 articles:
V. I. Kornilov, “Boundary-layer control on a body of revolution with a large aspect ratio by means of distributed air blowing”, Thermophys. Aeromech., 30:5 (2024), 819
V. I. Kornilov, A. N. Popkov, “State of the art and prospects of investigating the possibility of turbulent boundary layer control with the use of air blowing on a body of revolution (review)”, J. Appl. Mech. Tech. Phys., 65:2 (2024), 183–201
Citation in format AMSBIB
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