Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings

• 1. 飞机机翼上的机翼后缘控制面 [P] . 中国专利： CN100542889C . 2009.09.23
• 2. 飞机机翼上的先进机翼后缘控制面 [P] . 中国专利： CN101267980A . 2008-09-17
• 3. Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings [P] . 美国专利： US2005151029A1 . 2005-07-14

  机译： 使用超音速层流机翼的后缘控制面进行升力和扭转控制

• 4. WING WITH SUPERSONIC FREE LAMINAR FLOW (VERSIONS) AND WING SURFACE LAMINAR FLOW CONTROL SYSTEM [P] . 俄罗斯专利： RU2133692C1 . 1999-07-27

  机译： 具有超音速自由层流（版本）和机翼表面层流控制系统的机翼

• 5. Lifting device for remote or radio controlled aircraft, has anterior and posterior wings with trailing edges returning towards respective wing root in elliptical manner and in oval shape after curvature, respectively [P] . 法国专利： FR2850585A1 . 2004-08-06

  机译： 用于遥控或无线电遥控飞机的提升装置，具有前翼和后翼，其后缘分别以椭圆形和曲率弯曲后的椭圆形返回各自的翼根

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• 1. Modeling and Experiment of a Morphing Wing Integrated with a Trailing Edge Control Actuation System [J] . HE Yuanyuan ,GUO Shijun . 中国机械工程学报 . 2012,第002期
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• 3. 电机驱动柔性变体机翼后缘结构变形及控制研究 [A] . 常祺 . 2020