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Bifurcations in the transonic flow past a symmetric airfoil. / Kuz'min, A. G.

в: Fluid Dynamics, Том 41, № 4, 07.2006, стр. 629-632.

Результаты исследований: Научные публикации в периодических изданиях › статья › Рецензирование

Harvard

Kuz'min, AG 2006, 'Bifurcations in the transonic flow past a symmetric airfoil', Fluid Dynamics, Том. 41, № 4, стр. 629-632. https://doi.org/10.1007/s10697-006-0081-4

APA

Kuz'min, A. G. (2006). Bifurcations in the transonic flow past a symmetric airfoil. Fluid Dynamics, 41(4), 629-632. https://doi.org/10.1007/s10697-006-0081-4

Vancouver

Kuz'min AG. Bifurcations in the transonic flow past a symmetric airfoil. Fluid Dynamics. 2006 Июль;41(4):629-632. https://doi.org/10.1007/s10697-006-0081-4

Author

Kuz'min, A. G. / Bifurcations in the transonic flow past a symmetric airfoil. в: Fluid Dynamics. 2006 ; Том 41, № 4. стр. 629-632.

BibTeX

@article{b7cbf61de9dc48a2b7922fa570642274,
title = "Bifurcations in the transonic flow past a symmetric airfoil",
abstract = "Transonic flow past an airfoil with a small curvature in its midchord region is numerically investigated. The branching of the stationary solutions of the Euler equations is established and attributed to flow instability at certain angles of attack and freestream Mach numbers. The dependence of the lift coefficient on these parameters is studied.",
keywords = "Airfoil, Bifurcations, Instability, Local supersonic zones",
author = "Kuz'min, {A. G.}",
note = "Funding Information: The study was carried out with the support of the Russian Foundation for Basic Research (project No. 05-01-00529). The author wishes to thank A. V. Ivanova and K. V. Babarykin for assistance in calculations.",
year = "2006",
month = jul,
doi = "10.1007/s10697-006-0081-4",
language = "English",
volume = "41",
pages = "629--632",
journal = "Fluid Dynamics",
issn = "0015-4628",
publisher = "Springer Nature",
number = "4",

}

RIS

TY - JOUR

T1 - Bifurcations in the transonic flow past a symmetric airfoil

AU - Kuz'min, A. G.

N1 - Funding Information: The study was carried out with the support of the Russian Foundation for Basic Research (project No. 05-01-00529). The author wishes to thank A. V. Ivanova and K. V. Babarykin for assistance in calculations.

PY - 2006/7

Y1 - 2006/7

N2 - Transonic flow past an airfoil with a small curvature in its midchord region is numerically investigated. The branching of the stationary solutions of the Euler equations is established and attributed to flow instability at certain angles of attack and freestream Mach numbers. The dependence of the lift coefficient on these parameters is studied.

AB - Transonic flow past an airfoil with a small curvature in its midchord region is numerically investigated. The branching of the stationary solutions of the Euler equations is established and attributed to flow instability at certain angles of attack and freestream Mach numbers. The dependence of the lift coefficient on these parameters is studied.

KW - Airfoil

KW - Bifurcations

KW - Instability

KW - Local supersonic zones

UR - http://www.scopus.com/inward/record.url?scp=33750586737&partnerID=8YFLogxK

U2 - 10.1007/s10697-006-0081-4

DO - 10.1007/s10697-006-0081-4

M3 - Article

AN - SCOPUS:33750586737

VL - 41

SP - 629

EP - 632

JO - Fluid Dynamics

JF - Fluid Dynamics

SN - 0015-4628

IS - 4

ER -

ID: 98581079