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Published in: Fluid Dynamics 5/2020

01-09-2020

Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack

Authors: S. V. Guvernyuk, A. G. Kuzmin, M. M. Simonenko

Published in: Fluid Dynamics | Issue 5/2020

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Abstract—

The results of the numerical investigation of supersonic flow past a sharp slender body at an angle of attack are given with reference to the example of an axisymmetric cylindrical body with a conical nose. Separated and vortex structures developed at various angles of attack are identified. The effect of anomalous increase in pressure on the leeward side is explained.

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Literature
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go back to reference Petrov, K.P., Aerodinamika tel prosteishikh form (Simplest-Shape Body Aerodynamics), Moscow, Factorial, 1998. Petrov, K.P., Aerodinamika tel prosteishikh form (Simplest-Shape Body Aerodynamics), Moscow, Factorial, 1998.
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go back to reference Hemsch, M.J. and Nielsen, J.N., Tactical Missile Aerodynamics. Progress in Aeronautics and Astronautics, Ed by Hemsch, M.J. and Nielsen, J.N., New York: American Institute of Aeronautics and Astronautics, Inc., 1986. Vol. 104. Hemsch, M.J. and Nielsen, J.N., Tactical Missile Aerodynamics. Progress in Aeronautics and Astronautics, Ed by Hemsch, M.J. and Nielsen, J.N., New York: American Institute of Aeronautics and Astronautics, Inc., 1986. Vol. 104.
Metadata
Title
Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack
Authors
S. V. Guvernyuk
A. G. Kuzmin
M. M. Simonenko
Publication date
01-09-2020
Publisher
Pleiades Publishing
Published in
Fluid Dynamics / Issue 5/2020
Print ISSN: 0015-4628
Electronic ISSN: 1573-8507
DOI
https://doi.org/10.1134/S0015462820050080

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