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Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack. / Guvernyuk, S. V.; Kuzmin, A. G.; Simonenko, M. M.

In: Fluid Dynamics, Vol. 55, No. 5, 01.09.2020, p. 653-656.

Research output: Contribution to journal › Article › peer-review

Harvard

Guvernyuk, SV, Kuzmin, AG & Simonenko, MM 2020, 'Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack', Fluid Dynamics, vol. 55, no. 5, pp. 653-656. https://doi.org/10.1134/S0015462820050080

APA

Guvernyuk, S. V., Kuzmin, A. G., & Simonenko, M. M. (2020). Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack. Fluid Dynamics, 55(5), 653-656. https://doi.org/10.1134/S0015462820050080

Vancouver

Guvernyuk SV, Kuzmin AG, Simonenko MM. Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack. Fluid Dynamics. 2020 Sep 1;55(5):653-656. https://doi.org/10.1134/S0015462820050080

Author

Guvernyuk, S. V. ; Kuzmin, A. G. ; Simonenko, M. M. / Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack. In: Fluid Dynamics. 2020 ; Vol. 55, No. 5. pp. 653-656.

BibTeX

@article{7ef8957a51c045c29e21795c6fbb9287,
title = "Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack",
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.",
keywords = "angle of attack, flow separation, slender axisymmetric body, supersonic flow",
author = "Guvernyuk, {S. V.} and Kuzmin, {A. G.} and Simonenko, {M. M.}",
note = "Funding Information: The work was carried out with partial financial support from the Russian Foundation for Basic Research (project no. 19-01-00242). The calculations were performed using resources of the Computing Center of Saint Petersburg State University ( http://cc.spbu.ru ). Publisher Copyright: {\textcopyright} 2020, Pleiades Publishing, Ltd. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.",
year = "2020",
month = sep,
day = "1",
doi = "10.1134/S0015462820050080",
language = "English",
volume = "55",
pages = "653--656",
journal = "Fluid Dynamics",
issn = "0015-4628",
publisher = "Springer Nature",
number = "5",

}

RIS

TY - JOUR

T1 - Development of the Vortex Flow Structure on the Leeward Side of an Axisymmetric Body in Supersonic Free Stream at an Angle of Attack

AU - Guvernyuk, S. V.

AU - Kuzmin, A. G.

AU - Simonenko, M. M.

N1 - Funding Information: The work was carried out with partial financial support from the Russian Foundation for Basic Research (project no. 19-01-00242). The calculations were performed using resources of the Computing Center of Saint Petersburg State University ( http://cc.spbu.ru ). Publisher Copyright: © 2020, Pleiades Publishing, Ltd. Copyright: Copyright 2020 Elsevier B.V., All rights reserved.

PY - 2020/9/1

Y1 - 2020/9/1

N2 - 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.

AB - 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.

KW - angle of attack

KW - flow separation

KW - slender axisymmetric body

KW - supersonic flow

UR - http://www.scopus.com/inward/record.url?scp=85091301027&partnerID=8YFLogxK

U2 - 10.1134/S0015462820050080

DO - 10.1134/S0015462820050080

M3 - Article

AN - SCOPUS:85091301027

VL - 55

SP - 653

EP - 656

JO - Fluid Dynamics

JF - Fluid Dynamics

SN - 0015-4628

IS - 5

ER -

ID: 70201666