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Self-sustained oscillations and bifurcations of transonic flow past simple airfoils. / Kuz'min, A. G.

In: Journal of Applied Mechanics and Technical Physics, Vol. 49, No. 6, 2008, p. 919-925.

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

Harvard

Kuz'min, AG 2008, 'Self-sustained oscillations and bifurcations of transonic flow past simple airfoils', Journal of Applied Mechanics and Technical Physics, vol. 49, no. 6, pp. 919-925. https://doi.org/10.1007/s10808-008-0114-3

APA

Kuz'min, A. G. (2008). Self-sustained oscillations and bifurcations of transonic flow past simple airfoils. Journal of Applied Mechanics and Technical Physics, 49(6), 919-925. https://doi.org/10.1007/s10808-008-0114-3

Vancouver

Kuz'min AG. Self-sustained oscillations and bifurcations of transonic flow past simple airfoils. Journal of Applied Mechanics and Technical Physics. 2008;49(6):919-925. https://doi.org/10.1007/s10808-008-0114-3

Author

Kuz'min, A. G. / Self-sustained oscillations and bifurcations of transonic flow past simple airfoils. In: Journal of Applied Mechanics and Technical Physics. 2008 ; Vol. 49, No. 6. pp. 919-925.

BibTeX

@article{13d701dba2614c3a975fe4c7ce6970fb,
title = "Self-sustained oscillations and bifurcations of transonic flow past simple airfoils",
abstract = "A turbulent flow past two symmetric airfoils, whose bow and aft portions are circular arcs, whereas midparts are flat, is studies numerically. The amplitude of lift coefficient oscillations versus the free-stream Mach number M ∞ is analyzed at zero angle of attack. Ranges of M ∞ in which there exist flow bifurcations are determined.",
keywords = "Airfoil, Bifurcations, Buffet, Local supersonic zones, Shock waves",
author = "Kuz'min, {A. G.}",
year = "2008",
doi = "10.1007/s10808-008-0114-3",
language = "English",
volume = "49",
pages = "919--925",
journal = "Journal of Applied Mechanics and Technical Physics",
issn = "0021-8944",
publisher = "МАИК {"}Наука/Интерпериодика{"}",
number = "6",

}

RIS

TY - JOUR

T1 - Self-sustained oscillations and bifurcations of transonic flow past simple airfoils

AU - Kuz'min, A. G.

PY - 2008

Y1 - 2008

N2 - A turbulent flow past two symmetric airfoils, whose bow and aft portions are circular arcs, whereas midparts are flat, is studies numerically. The amplitude of lift coefficient oscillations versus the free-stream Mach number M ∞ is analyzed at zero angle of attack. Ranges of M ∞ in which there exist flow bifurcations are determined.

AB - A turbulent flow past two symmetric airfoils, whose bow and aft portions are circular arcs, whereas midparts are flat, is studies numerically. The amplitude of lift coefficient oscillations versus the free-stream Mach number M ∞ is analyzed at zero angle of attack. Ranges of M ∞ in which there exist flow bifurcations are determined.

KW - Airfoil

KW - Bifurcations

KW - Buffet

KW - Local supersonic zones

KW - Shock waves

UR - http://www.scopus.com/inward/record.url?scp=56749154658&partnerID=8YFLogxK

U2 - 10.1007/s10808-008-0114-3

DO - 10.1007/s10808-008-0114-3

M3 - Article

AN - SCOPUS:56749154658

VL - 49

SP - 919

EP - 925

JO - Journal of Applied Mechanics and Technical Physics

JF - Journal of Applied Mechanics and Technical Physics

SN - 0021-8944

IS - 6

ER -

ID: 98580920