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Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack

机译：攻角下细长锥的层流边界层分离的计算分析

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《AIAA Aerospace Sciences Meeting and Exhibit》|2005年|P.1-11|共11页
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J. Stecher; G. Candler;
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中图分类航空;
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1. Experimental investigation of the influence of the passive porous coating on laminar-turbulent transition of the hypersonic boundary layer of the sharp cone at angles of attack [J] . Sergey Morozov, Sergey Lukashevich, Alexander Shiplyuk MATEC Web of Conferences . 2017,第1期

机译：被动多孔涂层对尖锐锥形边界层层状湍流转变的实验研究
2. Hypersonic boundary-layer separation detection with pressure-sensitive paint for a cone at high angle of attack [J] . Running Carson L., Sakaue Hirotaka, Juliano Thomas J. Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2019,第1期

机译：高度边界层分离检测，具有高攻角锥体的压敏涂料
3. Stability Analysis of Hypersonic Boundary Layer over a Cone at Small Angle of Attack [J] . Feng Ji, Xunhua Liu, Qiang Wang, Advances in Mechanical Engineering . 2014,第Pta3期

机译：小攻角下圆锥体上超音速边界层的稳定性分析
4. Computational Analysis of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack [C] . American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting and Exhibit . 2005

机译：在攻角处纤细锥体上层边界层分离的计算分析
5. Hypersonic boundary-layer transition measurements at Mach 10 on a large seven-degree cone at angle of attack [D] . Moraru, Ciprian G. 2015

机译：在大七度锥面的迎角处以10马赫的高超声速边界层跃迁测量
6. Boundary layer control by a fish: Unsteady laminar boundary layers of rainbow trout swimming in turbulent flows [O] . Kazutaka Yanase, Pentti Saarenrinne 2016

机译：鱼的边界层控制：虹鳟在湍流中游荡的不稳定层流边界层
7. Experimental investigation of the influence of the passive porous coating on laminar-turbulent transition of the hypersonic boundary layer of the sharp cone at angles of attack [O] . Sergey Morozov, Sergey Lukashevich, Alexander Shiplyuk 2017

机译：被动多孔涂层对尖锐锥形边界层层状湍流转变的实验研究
8. Experimental Results of Laminar Boundary Layer Separation on a Slender Cone at Angle of Attack at M Infinity Equals 14.2. [R] . stetson,kenneth f. 1972

机译：m无限等于14.2的攻角下细长锥上层流边界层分离的实验结果。

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