Control device making it possible to vary the angle of attack of the wings of an airplane

• 1. 一种改善飞机大迎角俯仰特性的机翼后缘襟副翼使用方法 [P] . 中国专利： CN113562162A . 2021-10-29
• 2. 一种用于旋转机翼飞机中改变旋转机翼气动布局的装置 [P] . 中国专利： CN209757520U . 2019.12.10
• 3. Airplane to the surface and the angle of attack vary independently, its connections to the aircraft or plane, the devices for its operation, the instruments, the operation to make and to conduct the flat as it is necessary [P] . 法国专利： FR411786A . 1910-06-25

  机译： 飞机到水面和迎角的变化是独立的，它与飞机或飞机的连接，其操作设备，仪器，必要时进行制造和传导的操作

• 4. Devices to vary at rest or in Motion, the angle of attack (incidence) of the wings and Balancing the air machines. [P] . ES75847A1 . 1921-01-16

  机译： 可以在静止或运动，机翼的迎角（入射角）和气动设备平衡方面变化的设备。

• 5. Device for simultaneously and progressively varying the camber and the angle of attack of hydrodynamic and aerodynamic wings [P] . 美国专利： US10035579B2 . 2018-07-31

  机译： 用于同时逐步改变流体动力和空气动力机翼的外倾角和迎角的装置

• 1. COMPUTATION OF FIELD STRUCTURE AND AERODYNAMIC CHARACTERISTICS OF DELTA WINGS AT HIGH ANGLES OF ATTACK [J] . YANG Li-zhi, GAO Zheng-hong 应用数学和力学（英文版） . 2005,第006期
• 2. Control for Underactuated Reentry Aircraft in Small Angle of Attack [J] . Min Changwan, Wang Ying, Xiao Zhen, 南京航空航天大学学报（英文版） . 2017,第006期
• 3. Nose micro-blowing for asymmetric vortices control on blunt-nose slender body at high angle of attack [J] . Lei Wang, Yankui Wang, Zhongyang Qi 力学快报(英文版) . 2017,第006期
• 4. ASYMMETRIC VORTICES FLOW OVER SLENDER BODY AND ITS ACTIVE CONTROL AT HIGH ANGLE OF ATTACK [J] . DENG Xueying, WANG Yankui 力学学报：英文版 . 2004,第006期
• 5. Robust control of wing rock motion under time varying angle of attack using UDE [C] . Bellankimath Apurva, Chandar T.S. 2015 International Conference on Industrial Instrumentation and Control . 2015
• 6. Aerodynamic control of a wing at low angles of attack using synthetic jets and Gurney flaps. [D] . Shea, Patrick R. 2008
• 7. Associated factors of acute primary angle closure glaucoma in a sub-group of Chinese people: comparison between attack eyes and normal controls [O] . Lifang Liu, Xinyu Liu, Chukai Huang, -1
• 8. Behavior of Horseshoe Vortex at Wing/End Wall Junction with Attack Angle. 1st Report. Effect of Attack Angle on Mean Flow. [O] . Masahiko Yamamoto, Takaaki Shizawa, Shinji Honami 1995
• 9. Wind tunnel research comparing lateral control devices, particularly at high angles of attack X : various control devices on a wing with a fixed auxiliary airfoil [R] . Weick, Fred E, Noyes, Richard W 1933

• 1. Radio Controlled “3D Aerobatic Airplanes” as Basis for Fixed-Wing UAVs with VTOL Capability [J] . Chung-How Poh ,Chung-Kiak Poh . 应用科学（英文） . 2014,第12期
• 2. 低雷诺数小展弦比机翼的几何特征对于大迎角自激滚转影响的实验研究摘要 [C] . 胡天翔 ,张建军 ,刘沛清 . 北京力学会第二十二届学术年会 . 2016
• 3. 飞机大迎角非定常气动力建模和仿真研究 [A] . 王峥华 . 2010