Flow around a low-aspect-ratio wall-bounded 2D hydrofoil › Обзор исследований

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Flow around a low-aspect-ratio wall-bounded 2D hydrofoil : A LES/PIV study. / Dauengauer, E. I.; Mullyadzhanov, R. I.; Timoshevskiy, M. V. и др.

в: Journal of Physics: Conference Series, Том 1128, № 1, 012085, 07.12.2018.

Результаты исследований: Научные публикации в периодических изданиях › статья по материалам конференции › Рецензирование

Harvard

Dauengauer, EI, Mullyadzhanov, RI, Timoshevskiy, MV, Zapryagaev, II & Pervunin, KS 2018, 'Flow around a low-aspect-ratio wall-bounded 2D hydrofoil: A LES/PIV study', Journal of Physics: Conference Series, Том. 1128, № 1, 012085. https://doi.org/10.1088/1742-6596/1128/1/012085

APA

Dauengauer, E. I., Mullyadzhanov, R. I., Timoshevskiy, M. V., Zapryagaev, I. I., & Pervunin, K. S. (2018). Flow around a low-aspect-ratio wall-bounded 2D hydrofoil: A LES/PIV study. Journal of Physics: Conference Series, 1128(1), [012085]. https://doi.org/10.1088/1742-6596/1128/1/012085

Vancouver

Dauengauer EI, Mullyadzhanov RI, Timoshevskiy MV, Zapryagaev II, Pervunin KS. Flow around a low-aspect-ratio wall-bounded 2D hydrofoil: A LES/PIV study. Journal of Physics: Conference Series. 2018 дек. 7;1128(1):012085. doi: 10.1088/1742-6596/1128/1/012085

Author

Dauengauer, E. I. ; Mullyadzhanov, R. I. ; Timoshevskiy, M. V. и др. / Flow around a low-aspect-ratio wall-bounded 2D hydrofoil : A LES/PIV study. в: Journal of Physics: Conference Series. 2018 ; Том 1128, № 1.

BibTeX

@article{d8c5487c8c3c48c984b34acdf3e74880,

title = "Flow around a low-aspect-ratio wall-bounded 2D hydrofoil: A LES/PIV study",

abstract = "We performed Large-eddy simulations (LES) of the flow around a low-aspect-ratio wall-bounded 2D hydrofoil at the zero angle of attack using spectral-element method (SEM). The flow was considered for several Reynolds numbers ReC = 500, 5.0 × 103, 5.0 × 104 and 1.2 × 106 based on the foil chord to reveal the influence of the test channel sidewalls and viscous effects. The laminar-turbulent transition of the boundary layer was registered. A comparison of the numerical results with experimental data for the highest Reynolds number was performed and showed an excellent agreement.",

keywords = "DIRECT NUMERICAL-SIMULATION, LARGE-EDDY SIMULATION, SEPARATION, AIRFOIL",

author = "Dauengauer, {E. I.} and Mullyadzhanov, {R. I.} and Timoshevskiy, {M. V.} and Zapryagaev, {I. I.} and Pervunin, {K. S.}",

note = "Publisher Copyright: {\textcopyright} 2018 Institute of Physics Publishing. All rights reserved.; 3rd All-Russian Scientific Conference Thermophysics and Physical Hydrodynamics with the School for Young Scientists, TPH 2018 ; Conference date: 10-09-2018 Through 16-09-2018",

year = "2018",

month = dec,

day = "7",

doi = "10.1088/1742-6596/1128/1/012085",

language = "English",

volume = "1128",

journal = "Journal of Physics: Conference Series",

issn = "1742-6588",

publisher = "IOP Publishing Ltd.",

number = "1",

}

RIS

TY - JOUR

T1 - Flow around a low-aspect-ratio wall-bounded 2D hydrofoil

T2 - 3rd All-Russian Scientific Conference Thermophysics and Physical Hydrodynamics with the School for Young Scientists, TPH 2018

AU - Dauengauer, E. I.

AU - Mullyadzhanov, R. I.

AU - Timoshevskiy, M. V.

AU - Zapryagaev, I. I.

AU - Pervunin, K. S.

PY - 2018/12/7

Y1 - 2018/12/7

N2 - We performed Large-eddy simulations (LES) of the flow around a low-aspect-ratio wall-bounded 2D hydrofoil at the zero angle of attack using spectral-element method (SEM). The flow was considered for several Reynolds numbers ReC = 500, 5.0 × 103, 5.0 × 104 and 1.2 × 106 based on the foil chord to reveal the influence of the test channel sidewalls and viscous effects. The laminar-turbulent transition of the boundary layer was registered. A comparison of the numerical results with experimental data for the highest Reynolds number was performed and showed an excellent agreement.

AB - We performed Large-eddy simulations (LES) of the flow around a low-aspect-ratio wall-bounded 2D hydrofoil at the zero angle of attack using spectral-element method (SEM). The flow was considered for several Reynolds numbers ReC = 500, 5.0 × 103, 5.0 × 104 and 1.2 × 106 based on the foil chord to reveal the influence of the test channel sidewalls and viscous effects. The laminar-turbulent transition of the boundary layer was registered. A comparison of the numerical results with experimental data for the highest Reynolds number was performed and showed an excellent agreement.

KW - DIRECT NUMERICAL-SIMULATION

KW - LARGE-EDDY SIMULATION

KW - SEPARATION

KW - AIRFOIL

UR - http://www.scopus.com/inward/record.url?scp=85058624256&partnerID=8YFLogxK

U2 - 10.1088/1742-6596/1128/1/012085

DO - 10.1088/1742-6596/1128/1/012085

M3 - Conference article

AN - SCOPUS:85058624256

VL - 1128

JO - Journal of Physics: Conference Series

JF - Journal of Physics: Conference Series

SN - 1742-6588

IS - 1

M1 - 012085

Y2 - 10 September 2018 through 16 September 2018

ER -

ID: 17895311