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Stabilization of Helicopter Blades with Severed Pitch Links Using Trailing-Edge Flaps

机译：使用后缘襟翼稳定直立式叶片与切断螺距

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Roberto Celi;
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年度 2015
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1. Analysis of helicopter vibratory hub loads alleviation by cyclic trailing-edge blade flap actuation [J] . M. Gennaretti, M. Molica Colella, G. Bernardini Aeronautical journal . 2009,第1146期

机译：循环后缘叶片襟翼驱动减轻直升机振动轮毂载荷的分析
2. Pitching Airfoil with Combined Gurney Flap and Unsteady Trailing-Edge Flap Deflection [J] . T. Lee, Y. Y. Su AIAA Journal . 2012,第2期

机译：结合格尼襟翼和非定常后缘襟翼偏转的俯仰翼型
3. Vibration reduction of helicopter with trailing-edge flaps at various flying conditions [J] . Kodakkattu S. K., Joy M. L., Nair K. Prabhakaran Proceedings of the Institution of Mechanical Engineers . 2017,第G4期

机译：在各种飞行条件下，带后缘襟翼的直升机减震
4. Structural Design of an Active Trailing-Edge Flap Blade for Helicopter Vibration Control [C] . Balakumaran Natarajan, WonJong Eun, Jaehwan Lee, AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference . 2012

机译：用于直升机振动控制的主动后缘襟翼叶片的结构设计
5. Helicopter Rotor Smoothing with a Continuous Trailing-Edge Flap [D] . ?Ding, Lan 2020

机译：直升机旋翼平滑与连续尾缘襟翼
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. Small-Scale Helicopter Blade Flap-Lag Equations of Motion For A Flybarless Pitch-Lag-Flap Main Rotor [O] . Taamallah S. 2011

机译：无副翼俯仰滞后襟翼主旋翼的小型直升机叶片襟翼滞后运动方程
8. Theoretical Analysis of Linked Leading- Edge and Trailing-Edge Flap-Type Controls [R] . Yates, E. C. 1956

机译：连杆前缘和后缘襟翼式控制器的理论分析

Stabilization of Helicopter Blades with Severed Pitch Links Using Trailing-Edge Flaps

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