Natural Transition in Supersonic Flows: Flat Plate, Swept Cylinder, Swept Wing

机译：超声速流动的自然过渡：平板，后掠圆柱体，后掠翼

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《AIAA Fluid Dynamics Conference;AIAA Flow Control Conference;AIAA Thermophysics Conference;AIAA Plasmadynamics and Lasers Conference》|2004年|P.1-10|共10页
会议地点 Portland, OR(US);Portland, OR(US);Portland, OR(US);Portland, OR(US)
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J. Archambaud; F. Louis; A. Seraudie; D. Arnal; G. Carrier;
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ONERA Toulouse France;

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1. Effect of unit Reynolds number on the laminar-turbulent transition on a swept wing in supersonic flow [J] . Yu.G. Ermolaev, A.D. Kosinov, A.N. Semenov, Thermophysics and Aeromechanics . 2018,第5期

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2. STABILITY AND TRANSITION ON A SWEPT CYLINDER IN A SUPERSONIC FLOW [J] . A. I. Semisynov, A. V. Fedorov, V. E. Novikov, Journal of Applied Mechanics and Technical Physics . 2003,第2期

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3. The influence of moderate angle-of-attack variation on disturbances evolution and transition to turbulence in supersonic boundary layer on swept wing [J] . Kosinov Alexander, Semionov Nikolai, Yermolaev Yury, Proceedings of the Institution of Mechanical Engineers . 2020,第1期

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4. Natural Transition in Supersonic Flows: Flat Plate, Swept Cylinder, Swept Wing [C] . AIAA Fluid Dynamics Conference . 2004

机译：超音速流动的自然过渡：平板，扫缸，扫翼
5. Investigation of the Flowfield Downstream of a Discontinuous Backward-Facing Step on a Swept Flat Plate [D] . Yoshida, William. 2020

机译：在扫堤平板上的不连续反向落后步骤下游的流域研究
6. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows [O] . X. Gao, G. X. Xiang, W. J. Tang, -1

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7. The influence of moderate angle-of-attack variation on disturbances evolution and transition to turbulence in supersonic boundary layer on swept wing [O] . Alexander Kosinov, Nikolai Semionov, Yury Yermolaev, 2019

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8. Some Accurate Solutions of the Problem of Natural Vibrations of a Swept-Back Wing in a Supersonic Flow of Gas [R] . Lyubimov, V. M. 1963

机译：气体超音速流中后掠翼自然振动问题的一些精确解

Natural Transition in Supersonic Flows: Flat Plate, Swept Cylinder, Swept Wing

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