Supersonic airfoil with boundary layer control

• 1. 具有形成层流边界层流动的系统的飞机机翼 [P] . 中国专利： CN104703878B . 2016.08.24
• 2. 具有形成层流边界层流动的系统的飞机机翼 [P] . 中国专利： CN104703878A . 2015-06-10
• 3. BOUNDARY LAYER CONTROL ASSEMBLY FOR AN AIRCRAFT AIRFOIL AND METHOD OF CONTROLLING A BOUNDARY LAYER [P] . 美国专利： US2016221664A1 . 2016-08-04

  机译： 飞机机翼的边界层控制组件和控制边界层的方法

• 4. BOUNDARY LAYER CONTROL ASSEMBLY FOR AN AIRCRAFT AIRFOIL AND METHOD OF CONTROLLING A BOUNDARY LAYER [P] . 欧洲知识产权局专利： EP3050797A1 . 2016-08-03

  机译： 飞机机翼的边界层控制组件和控制边界层的方法

• 5. Controlling the boundary layer of an airfoil [P] . 美国专利： US8251319B2 . 2012-08-28

  机译： 控制翼型的边界层

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