Improvements relate to devices intended to increase the lifting force of the wings and the adjustment flaps

• 1. 用于调节增升襟翼的调节装置以及包括这种调节装置的机翼 [P] . 中国专利： CN101484355B . 2013.08.21
• 2. 用于调节增升襟翼的调节装置以及包括这种调节装置的机翼 [P] . 中国专利： CN101484355A . 2009-07-15
• 3. REGULATING DEVICE FOR ADJUSTMENT increases the lift of the wing flaps and the aerodynamic wing comprising such a control device [P] . 俄罗斯专利： RU2009102946A . 2010-08-10

  机译： 调节装置增加了包括这种控制装置的机翼襟翼和气动机翼的升力。

• 4. Aircraft wing with articulated flaps - has main and auxiliary flap systems pivoted and actuated for increasing the lift force [P] . 德国专利： DE2054150C3 . 1975-10-09

  机译： 带铰接襟翼的飞机机翼-具有枢转和致动的主副翼系统，以增加升力

• 5. Aircraft wing with articulated flaps - has main and auxiliary flap systems pivoted and actuated for increasing the lift force [P] . 德国专利： DE2054150B2 . 1975-03-06

  机译： 带铰接襟翼的飞机机翼-具有枢转和致动的主副翼系统，以增加升力

• 1. Aerodynamic mechanism of forces generated by twisting model-wing in bat flapping flight [J] . 管子武, 余永亮 应用数学和力学（英文版） . 2014,第012期
• 2. Control of flight forces and moments by flapping wings of model bumblebee [J] . WU Jiang-hao, SUN Mao 应用数学和力学（英文版） . 2008,第003期
• 3. Effects of unsteady deformation of flapping wing on its aerodynamic forces [J] . DU Gang, SUN Mao 应用数学和力学（英文版） . 2008,第006期
• 4. Effects of unsteady deformation of flapping wing on its aerodynamic forces [J] . 杜刚, 孙茂 应用数学和力学：英文版 . 2008,第006期
• 5. Evaluation of the aerodynamic performance increase thanks to a morphing A320 wing with high-lift flap by means of CFD Hi-Fi approaches [C] . A. Marouf, Y. Hoarau, J.B. Vos, AIAA aviation forum . 2019
• 6. Flapping wing devices for Mars exploration: Preliminary results from a novel flapping wing mechanism. [D] . Ania, Asier. 2009
• 7. Outperforming hummingbirds’ load-lifting capability with a lightweight hummingbird-like flapping-wing mechanism [O] . Frederik Leys, Dominiek Reynaerts, Dirk Vandepitte 2016
• 8. Optimization of lift force for a bio-inspired flapping wing model in hovering flight [O] . Zhang, H, Wen, C, Yang, A 2016
• 9. Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6). [R] . Lange, Roy H, May, Ralph W , Jr 1948

• 1. Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion [J] . Chunjin Yu ,Daewon Kim ,Yi Zhao . 应用数学与应用物理（英文） . 2014,第12期
• 2. 半展长襟翼梯形翼高升力构型的超大规模数值模拟 [C] . Wang Yuntao ,王运涛 ,Hong Junwu . 2015全国高性能计算学术年会 . 2015
• 3. 零航速下襟翼鳍升力建模与控制研究 [A] . 黄丹 . 2010