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Flight Test Results of a Trailing Edge Flap Designed for Direct-Lift Control

机译：设计用于直接提升控制的后缘襟翼的飞行测试结果

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作者
Taylor, C. R.;
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年度 1969
页码 p.1-84
总页数 84
原文格式 PDF
正文语种 eng
中图分类
关键词
Boundary layers ; Flight tests ; Trailing-edge flaps ; Aerodynamic characteristics ; Deceleration ; Jet impingement;

机译：边界层;飞行试验;后缘襟翼;空气动力学特性;减速度;射流冲击;

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专利

1. Design, Development, and Hover Testing of a Mach-Scale Swashplateless Rotor Using Brushless DC Motor-Actuated Trailing Edge Flaps for Rotor Primary Control [J] . Saxena Anand, Chopra Inderjit Journal of the American Helicopter Society . 2017,第2期

机译：使用无刷直流电动机驱动的后缘襟翼的马赫级无旋转斜盘转子的设计，开发和悬停测试，用于转子主控制
2. Wind-Tunnel Testing of Rotor with Individually Controlled Trailing-Edge Flaps for Vibration Reduction [J] . Beatrice Roget, Inderjit Chopra Journal of Aircraft . 2008,第3期

机译：带有独立控制后缘襟翼的转子风洞测试，用于减振
3. In-Flight Rotorblade Tracking Control for Helicopters Using Active Trailing-Edge Flaps [J] . F. A. King, J.-B. Maurice, W. Fichter, Journal of guidance, control, and dynamics . 2014,第2期

机译：使用主动后缘襟翼的直升机飞行中旋翼桨叶跟踪控制
4. Flight Testing of a Model Aircraft with Trailing- Edge Flaps Optimized for Lift Distribution Control [C] . N. Guerreiro, J. Hubbard AIAA guidance, navigation and control conference and exhibit . 2008

机译：对后缘襟翼进行了升力分布控制优化的模型飞机的飞行测试
5. Design and Construction of a Wind Tunnel Model with Active Variable Camber Continuous Trailing Edge Flap for Aeroelastic 'In-flight' Shape Optimization Tests [D] . Precup, Nathan 2018

机译：主动可变弯度连续后缘襟翼风洞模型的设计与构建，用于气动弹性“飞行中”形状优化测试
6. Trailing-Edge Flap Control for Mitigating Rotor Power Fluctuations of a Large-Scale Offshore Floating Wind Turbine under the Turbulent Wind Condition [O] . Bofeng Xu, Junheng Feng, Tongguang Wang, 2018

机译：湍流风能下用于减轻大型近海浮动风力涡轮机的转子电力波动的后缘襟翼控制
7. Design, manufacturing and testing of Controllable Rubber Trailing Edge Flaps [O] . Løgstrup Andersen Tom, Aagaard Madsen Helge, Barlas Thanasis K, 2015

机译：可控橡胶后缘襟翼的设计，制造和测试
8. Flight test results of a trailing edge flap designed for direct-lift control [R] . Taylor, C. R., Jr. 1969

机译：设计用于直接升力控制的后缘襟翼的飞行试验结果

Flight Test Results of a Trailing Edge Flap Designed for Direct-Lift Control

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