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An experimental investigation of support strut interference on a three-percent fighter model at high angles of attack

机译：高攻角下百分之三的战斗机模型支撑支柱干扰的实验研究

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http://archive.org/details/experimentalinve00somm

机译：HTTP://archive.org/details/experimental in VE00so MM

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作者
Sommers John Douglas.;
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年度 1989
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原文格式 PDF
正文语种 en_US
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专利

1. Investigation of Support Interference in High-Angle-of-Attack Testing [J] . G. S. Taylor, I. Gursul, D. I. Greenwell Journal of Aircraft . 2003,第1期

机译：高攻角测试中支持干扰的调查
2. A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model [J] . P. J. Attar, E. H. Dowell, D. M. Tang Journal of Fluids and Structures . 2003,第2期

机译：稳定迎角对三角翼板模型非线性颤动影响的理论和实验研究
3. Experimental study on aerodynamic noise generated from two-dimensional models (2nd report, effect of the angle of inclination of circular cylinders and the angle of attack of square cylinders to aerodynamic noise) [J] . Shoji Yamada, Hajime Fujita, Yosiyuki Maruta 日本機械学会論文集. B編 . 1997,第610期

机译：二维模型产生的空气动力噪声的实验研究（第二次报告，圆柱倾斜角和方形圆柱的迎角对空气动力噪声的影响）
4. An Investigation of Support Interference in High Angle of Attack Testing [C] . G. Taylor, I. Gursul, D. Greenwell Aerospace Sciences Meeting and Exhibit . 2003

机译：高攻角测试中支持干扰的研究
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. Axial stent strut angle influences wall shear stress after stent implantation: analysis using 3D computational fluid dynamics models of stent foreshortening [O] . John F LaDisa Jr, Lars E Olson, Douglas A Hettrick, 2005

机译：轴向支架撑杆角度影响支架植入后的壁切应力：使用支架缩短的3D计算流体动力学模型进行分析
7. Hot-wire surveys in the vortex wake downstream of a three-percent fighter aircraft model at high angles of attack [O] . Frink William D. Jr. 1990

机译：在高攻角下，百分之三的战斗机模型下游的涡流中进行的热线测量

An experimental investigation of support strut interference on a three-percent fighter model at high angles of attack

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