Improvement in modificacao geometry of the wing planes in flight, the wing structure without interference.

• 1. 一种基于类别形状函数变换的可变形机翼的快速几何建模方法 [P] . 中国专利： CN113536458A . 2021-10-22
• 2. 高空飞行器机翼几何形状 [P] . 中国专利： CN107567415A . 2018-01-09
• 3. Modificacao geometry of the wing planes in flight, the wing structure without interference. [P] . BR5901643U . 1981-06-09

  机译： 机翼在飞行过程中几何变形，机翼结构无干扰。

• 4. Modificacao geometry of the wing planes in flight, the wing structure without interference. [P] . BR5900633U . 1979-09-25

  机译： 机翼在飞行过程中几何变形，机翼结构无干扰。

• 5. device for regulating continues during the flight, the inclinazionedella wing structure in a plane type lightweight commute. [P] . IT1259710B . 1996-03-25

  机译： 在飞行过程中，用于调节的装置继续进行，在飞机型轻型通勤中，倾斜的机翼的机翼结构。

• 1. Improvement of Artificial Foldable Wing Models by Mimicking the Unfolding/Folding Mechanism of a Beetle Hind Wing [J] . Azhar Muhammad, Quoc Viet Nguyen, Hoon Cheol Park, 仿生工程学报（英文版） . 2010,第002期
• 2. Kinematics,Deformation,and Aerodynamics of a Flexible Flapping Rotary Wing in Hovering Flight [J] . Chao Zhou, Jianghao Wu 仿生工程学报（英文版） . 2021,第001期
• 3. A fault-tolerant control method for distributed flight control system facing wing damage [J] . CUI Yuwei, LI Aijun, MENG Xianfeng 系统工程与电子技术（英文版） . 2021,第005期
• 4. Fixed-wing UAV guidance law for ground target over-flight tracking [J] . ZHANG Min, ZHENG Chenming, HUANG Kun 系统工程与电子技术（英文版） . 2019,第002期
• 5. Control Device Studies for Yaw Control without Vertical Tail Plane on a 53° Swept Flying Wing Configuration [C] . Patrick Loechert, Kerstin C. Huber, Carsten M. Liersch, AIAA applied aerodynamics conference;AIAA aviation forum . 2018
• 6. Real-time non-linear flight control of a fixed-wing UAV =REAL-TIME NON-LINEAR FLIGHT CONTROL OF A FIXED-WING UAV [D] . Landry, Mario. 2012
• 7. Improvement of the aerodynamic performance by wing flexibility and elytra–hind wing interaction of a beetle during forward flight [O] . Tuyen Quang Le, Tien Van Truong, Soo Hyung Park, 2013
• 8. The Study of Development to Micro Flapping Robot Without Tail-Plane and Effect of its Wing Behavior for the Flight [O] . 井村 忠継 2012
• 9. Transonic flight tests to compare the zero-lift drags of 45 degree sweptback wings of aspect ratio 3.55 and 6.0 with and without nacelles at the wing tips [R] . Hoffman, Sherwood, Mapp, Richard C , Jr 1952

• 1. Design and Optimization of Wing Structure for a Fixed-Wing Unmanned Aerial Vehicle (UAV) [J] . Jiawen Yu . 现代机械工程（英文） . 2018,第4期
• 2. 平面形状和弹性对小展弦比机翼升力特性的影响 [C] . 左林玄 ,王晋军 . 第七届全国实验流体力学学术会议 . 2007
• 3. 基于形状记忆合金的变体机翼结构设计与实验研究 [A] . 杨金川 . 2020