Abstract
The chapter presents the results of numerical simulation of two-dimensional laminar flows near a regular system of cylinders, forming a plane lattice perpendicular to the velocity vector of the oncoming supersonic flow. A multiblock computing technology is applied using local curvilinear grids adapted to the surface of bodies and having finite areas of overlap with a global rectangular grid. The viscous boundary layers are resolved on the local grids using Navier–Stokes equations. The interaction of shock-wave structures and aerodynamic wakes behind the elements of the lattice is described within Euler equations. With a sequential increase and decrease in Mach number of the oncoming flow, several rearrangements of the flow structure near the grid are found. A multiple hysteresis was revealed, which is expressed in the fact that the flow structure and aerodynamic loads on the lattice elements depend not only on Mach number but also on the history of its change.
Access this chapter
Tax calculation will be finalised at checkout
Purchases are for personal use only
References
Guvernyuk, S.V.: On hypersonic flow around bodies with wire screens. Gas Wave Dyn. 4, 236–242 (in Russian) (2005)
Fomin, V.M., Mironov, S.G., Serdyuk, K.M.: Reducing the wave drag of bodies in supersonic flows using porous materials. Tech. Phys. Lett. 35(2), 117–119 (2009)
Kirilovskiy, S.V., Maslov, A.A., Mironov, S.G., Poplavskaya, T.V.: Application of the skeleton model of a highly porous cellular material in modeling supersonic flow past a cylinder with a forward gas-permeable insert. Fluid Dyn. 53(3), 409–416 (2018)
Maksimov, F.A.: Supersonic body wrapping. Comput. Res. Model. 5(6), 969–980 (in Russian) (2013)
Kudryavsev, A.N., Epshtein, D.B.: Hysteresis phenomenon in supersonic flow past a system of cylinders. Fluid Dyn. 47(3), 395–402 (2012)
Guvernyuk, S.V., Maksimov, F.A.: Supersonic flow past a flat lattice of cylindrical rods. Comput. Math. Math. Phys. 56(6), 1012–1019 (2016)
Guvernyuk, S.V., Savinov, K.G., Ul’yanov, G.S.: Supersonic flow round blunt perforated screens. Fluid Dyn. 20(1), 124–129 (1985)
Maksimov, F.A., Churakov, D.A., Shevelev, Y.D.: Development of mathematical models and numerical methods for aerodynamic design on multiprocessor computers. Comput. Math. Math. Phys. 51(2), 284–307 (2011)
Isaev, S.A., Baranov, P.A., Usachov, A.E.: Multiblock Computing Technologies in VP2/3 Aerothermodynamics Package. LAP LAMBERT Academic Publishing, Saarbryuken (in Russian) (2013)
Acknowledgements
The work was carried out with a partial financial support of the Russian Foundation for Basic Research (Project No. 19-01-00242) and partially under the state task of the ICAD RAS.
The calculations were carried out on MVS-100 K at Interdepartmental supercomputer center of the Russian Academy of Sciences.
Author information
Authors and Affiliations
Corresponding author
Editor information
Editors and Affiliations
Rights and permissions
Copyright information
© 2020 Springer Nature Singapore Pte Ltd.
About this paper
Cite this paper
Guvernyuk, S.V., Maksimov, F.A. (2020). On Structures of Supersonic Flow Around Plane System of Cylindrical Rods. In: Jain, L., Favorskaya, M., Nikitin, I., Reviznikov, D. (eds) Advances in Theory and Practice of Computational Mechanics. Smart Innovation, Systems and Technologies, vol 173. Springer, Singapore. https://doi.org/10.1007/978-981-15-2600-8_5
Download citation
DOI: https://doi.org/10.1007/978-981-15-2600-8_5
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-15-2599-5
Online ISBN: 978-981-15-2600-8
eBook Packages: Intelligent Technologies and RoboticsIntelligent Technologies and Robotics (R0)