Aircraft with wing of the supporting device for influencing the boundary layer

• 1. 带有机翼以及使不稳定流动状态的影响最小化的系统的飞机 [P] . 中国专利： CN103201172B . 2016.08.10
• 2. 带有机翼以及使不稳定流动状态的影响最小化的系统的飞机 [P] . 中国专利： CN103201172A . 2013-07-10
• 3. Aerodynamic component e.g. vertical tail of aircraft, for influencing air boundary layer, has outer layer influencing air boundary layer with openings, and air-permeable coupling layer provided between outer layer and supporting structure [P] . 德国专利： DE102010063769A1 . 2012-06-21

  机译： 空气动力学组件飞机的垂直尾翼，用于影响空气边界层，其外层具有影响开口的空气边界层，在该外层与支撑结构之间设置有透气耦合层

• 4. Device for the boundary layers influencing to the aircraft supporting force flue [P] . 德国专利： DE729879C . 1943-01-04

  机译： 用于影响飞机支撑力烟道的边界层的装置

• 5. Boundary layer influencing method for aircraft wings [P] . 德国专利： DE19703766C1 . 1998-03-26

  机译： 飞机机翼的边界层影响方法

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• 3. Influence of Warm Oxide Layer on Wettability and Contact Angle for Heat Transport Devices [J] . A. Takemura, K. Yuki, A. Sadayuki 机械工程与自动化：英文版 . 2017,第007期
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• 6. An immersed boundary method for simulating the effects of control devices used in mitigating shock/boundary-layer interactions. [D] . Ghosh, Santanu. 2010
• 7. An Improved Gaussian Mixture Model for Damage Propagation Monitoring of an Aircraft Wing Spar under Changing Structural Boundary Conditions [O] . Lei Qiu, Shenfang Yuan, Hanfei Mei, 2016
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• 9. Control of Transition in Swept-Wing Boundary Layers using MEMS Devices as Distributed Roughness [R] . Saric, W. S. 2001

• 1. Influence of PVK:NPB hole transporting layer on the characteristics of organic light-emitting devices [J] . WEN Wen YU Jun-sheng LI Lu MA Tao TANG Xiao-qing JIANG Ya-dong . 光电子快报：英文版 . 2008,第3期
• 2. 飞机机翼表面结冰对机翼气动性能的影响 [C] . 杨曦 ,张大林 . 中国航空学会人体工程、航医、救生专业委员会第六届学术年会 . 2003
• 3. 马赫数、攻角及后掠角对后掠机翼边界层稳定性及转捩的影响 [A] . 孙朋朋 . 2014