Enviar artigo por via de e-mail TRANSITION OF SUPERSONIC BOUNDARY LAYER OVER AN UPSWEPT WING DUE TO ACOUSTIC NOISE
- Autores: Chuvakhov P.V.1,2, Egorov I.V.1,2
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Afiliações:
- Central Aerohydrodynamic Institute named after Prof. N.E. Zhukovsky
- Moscow Institute of Physics and Technology
- Edição: Volume 509, Nº 1 (2023)
- Páginas: 63-66
- Seção: МЕХАНИКА
- URL: https://vietnamjournal.ru/2686-7400/article/view/651883
- DOI: https://doi.org/10.31857/S2686740023020050
- EDN: https://elibrary.ru/UPCMFS
- ID: 651883
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Resumo
Results of direct numerical simulation of the receptivity of the supersonic boundary layer over an upswept wing with a thin parabolic profile to acoustic noise of various intensity are presented. Acoustic noise is shown to be capable of triggering laminar-turbulent transition over the upswept wing of supersonic transport.
Sobre autores
P. Chuvakhov
Central Aerohydrodynamic Institute named after Prof. N.E. Zhukovsky; Moscow Institute of Physics and Technology
Autor responsável pela correspondência
Email: pavel_chuvahov@mail.ru
Russia, Moscow Region, Zhukovsky; Russia, Moscow Region, Dolgoprudny
I. Egorov
Central Aerohydrodynamic Institute named after Prof. N.E. Zhukovsky; Moscow Institute of Physics and Technology
Autor responsável pela correspondência
Email: i_v_egorov@mail.ru
Russia, Moscow Region, Zhukovsky; Russia, Moscow Region, Dolgoprudny
Bibliografia
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- Егоров И.В., Новиков А.В. Прямое численное моделирование ламинарно-турбулентного обтекания плоской пластины при гиперзвуковых скоростях потока // ЖВМиМФ. 2016. Т. 56. № 6. С. 1064–1081.
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