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A Flow Visualization Study of LEX Generated Vortices on a Scale Model of a F/A-18 Fighter Aircraft at High Angles of Attack

机译：F / A-18战斗机在高攻角比例模型上LEX产生涡流的流动可视化研究

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Approved for public release; distribution is unlimited.

机译：批准公开发布；发行是无限的。

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Cavazos Odilon V. Jr.;
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年度 1990
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专利

1. Microblowing for High-Angle-of-Attack Vortex Flow Control on a Fighter Aircraft [J] . Frederick W. Roos Journal of Aircraft . 2001,第3期

机译：用于战斗机的高攻击角涡流控制的微吹
2. Dragonfly flight: free-flight and tethered flow visualizations reveal a diverse array of unsteady lift-generating mechanisms, controlled primarily via angle of attack [J] . Thomas AL, Taylor GK, Srygley RB, The Journal of Experimental Biology . 2004,第Pta24期

机译：蜻蜓飞行：自由飞行和束缚流可视化显示各种不稳定的升力产生机制，这些机制主要通过迎角来控制
3. Dragonfly flight: free-flight and tethered flow visualizations reveal a diverse array of unsteady lift-generating mechanisms, controlled primarily via angle of attack [J] . Thomas ALR, Taylor GK, Srygley RB, The Journal of Experimental Biology . 2004,第24期

机译：蜻蜓飞行：自由飞行和束缚流可视化显示各种不稳定的升力产生机制，这些机制主要通过迎角来控制
4. Installed F/A-18 Inlet Flow Calculation at 30 deg Angle-of-Attack: A Comparative Study [C] . C.F.Smith, S.D.Podleski 30th AIAA/ASME/SAE/ASEE Joint Propulsion Conference June 27-29, 1994/Indianapolis, IN . -1

机译：攻击角为30度时安装的F / A-18进气流量计算：比较研究
5. Reconfigurable flight control for high angle of attack fighter aircraft, with wind tunnel study [D] . Siddiqui, Bilal Ahmed 2010

机译：高攻角战斗机的可重构飞行控制，带有风洞研究
6. Dynamic modeling of uteroplacental blood flow in IUGR indicates vortices and elevated pressure in the intervillous space – a pilot study [O] . Christian J. Roth, Eva Haeussner, Tanja Ruebelmann, -1

机译：IUGR子宫胎盘血流的动态模型表明小肠间隙存在涡旋和压力升高–一项初步研究
7. Flow visualization of the effect of pitch rate on the vortex development on the scale model of a F-18 fighter aircraft. [O] . Park Sung-Nam 1989

机译：F-18战斗机比例模型上的俯仰率对涡旋发展影响的流动可视化。

A Flow Visualization Study of LEX Generated Vortices on a Scale Model of a F/A-18 Fighter Aircraft at High Angles of Attack

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