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Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack. / Кузьмин, Александр Григорьевич; Бабарыкин, Константин Валентинович.

в: AIP Conference Proceedings, Том 2953, 060005, 20.11.2023.

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

Harvard

Кузьмин, АГ & Бабарыкин, КВ 2023, 'Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack', AIP Conference Proceedings, Том. 2953, 060005. https://doi.org/10.1063/5.0177488

APA

Кузьмин, А. Г., & Бабарыкин, К. В. (2023). Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack. AIP Conference Proceedings, 2953, [060005]. https://doi.org/10.1063/5.0177488

Vancouver

Кузьмин АГ, Бабарыкин КВ. Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack. AIP Conference Proceedings. 2023 Нояб. 20;2953. 060005. https://doi.org/10.1063/5.0177488

Author

Кузьмин, Александр Григорьевич ; Бабарыкин, Константин Валентинович. / Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack. в: AIP Conference Proceedings. 2023 ; Том 2953.

BibTeX

@article{0605c7178db9423a81bd5faeb00b6598,
title = "Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack",
abstract = "Numerical simulations of 3D turbulent flow over a projectile model have been performed at the angles of attack α = 4° and α = 6° at high subsonic free-stream Mach numbers M∞. The simulations are based on the unsteady Reynolds-averaged Navier-Stokes equations using the k-ω Shear Stress Transport and Detached Eddy Simulation turbulence models. The obtained solutions reveal an intricate behavior of the lift force and pitching moment as functions of M∞. Locations of shock waves and supersonic regions on the projectile are discussed, and a physical interpretation of two discontinuities in the dependence of aerodynamic coefficients on M∞ is suggested.",
author = "Кузьмин, {Александр Григорьевич} and Бабарыкин, {Константин Валентинович}",
year = "2023",
month = nov,
day = "20",
doi = "10.1063/5.0177488",
language = "English",
volume = "2953",
journal = "AIP Conference Proceedings",
issn = "0094-243X",
publisher = "American Institute of Physics",
note = "Fourteenth Conference of the Euro-American Consortium for Promoting the Application of Mathematics in Technical and Natural Sciences, AMiTaNS 2022 ; Conference date: 22-06-2022 Through 27-06-2022",
url = "http://2022.eac4amitans.eu/",

}

RIS

TY - JOUR

T1 - Peculiarities of aerodynamic loads on a projectile in transonic flight at small angles of attack

AU - Кузьмин, Александр Григорьевич

AU - Бабарыкин, Константин Валентинович

PY - 2023/11/20

Y1 - 2023/11/20

N2 - Numerical simulations of 3D turbulent flow over a projectile model have been performed at the angles of attack α = 4° and α = 6° at high subsonic free-stream Mach numbers M∞. The simulations are based on the unsteady Reynolds-averaged Navier-Stokes equations using the k-ω Shear Stress Transport and Detached Eddy Simulation turbulence models. The obtained solutions reveal an intricate behavior of the lift force and pitching moment as functions of M∞. Locations of shock waves and supersonic regions on the projectile are discussed, and a physical interpretation of two discontinuities in the dependence of aerodynamic coefficients on M∞ is suggested.

AB - Numerical simulations of 3D turbulent flow over a projectile model have been performed at the angles of attack α = 4° and α = 6° at high subsonic free-stream Mach numbers M∞. The simulations are based on the unsteady Reynolds-averaged Navier-Stokes equations using the k-ω Shear Stress Transport and Detached Eddy Simulation turbulence models. The obtained solutions reveal an intricate behavior of the lift force and pitching moment as functions of M∞. Locations of shock waves and supersonic regions on the projectile are discussed, and a physical interpretation of two discontinuities in the dependence of aerodynamic coefficients on M∞ is suggested.

UR - https://www.mendeley.com/catalogue/630279f0-d137-3e64-abe9-00e2aebe30cd/

U2 - 10.1063/5.0177488

DO - 10.1063/5.0177488

M3 - Conference article

VL - 2953

JO - AIP Conference Proceedings

JF - AIP Conference Proceedings

SN - 0094-243X

M1 - 060005

T2 - Fourteenth Conference of the Euro-American Consortium for Promoting the Application of Mathematics in Technical and Natural Sciences

Y2 - 22 June 2022 through 27 June 2022

ER -

ID: 114177605