Airfoil and boundary-layer control rotor

• 1. 一种大型低速翼型风洞侧壁边界层控制系统 [P] . 中国专利： CN108120582A . 2018-06-05
• 2. 操纵横跨风力涡轮机转子叶片的空气的边界层的主动流动控制系统和方法 [P] . 中国专利： CN102562461B . 2016.07.06
• 3. Method for controlling rotorcraft airfoil to minimize auxiliary rotor noise and enhance rotorcraft performance [P] . 美国专利： US9725164B2 . 2017-08-08

  机译： 控制旋翼机翼型以最小化辅助旋翼噪声并增强旋翼机性能的方法

• 4. Active control of multi-element rotor blade airfoils [P] . 美国专利： US6932569B2 . 2005-08-23

  机译： 主动控制多元素转子叶片翼型

• 5. ACTIVE CONTROL OF MULTI-ELEMENT ROTOR BLADE AIRFOILS [P] . 美国专利： US2005042091A1 . 2005-02-24

  机译： 主动式多叶片桨叶的主动控制

• 1. Adaptive rotor current control for wind-turbine driven DFIG using resonant controllers in a rotor rotating reference frame [J] . 浙江大学学报（英文版）（A辑：应用物理和工程） . 2008,第002期
• 2. Highly-Efficient Aerodynamic Optimal Design of Rotor Airfoil Using Viscous Adjoint Method [J] . Wu Qi, Zhao Qijun, Wang Qing 南京航空航天大学学报（英文版） . 2017,第002期
• 3. Vortex dynamics over an airfoil controlled by a nanosecond pulse discharge plasma actuator at low wind speed [J] . Hai DU, Lei WANG, Wenjie KONG, 等离子体科学和技术（英文版） . 2019,第012期
• 4. Magnetic Field Analysis of Interior Composite-Rotor Controllable-Flux Permanent Magnet Synchronous Machine [J] . CHEN Yiguang, PAN Wei, SHEN Yonghuan, 天津大学学报（英文版） . 2006,第005期
• 5. A study of EV induction motor controller based on rotor flux oriented control [J] . Song Jianguo, Chen Quanshi 高技术通讯（英文版） . 2006,第002期
• 6. Airfoil Boundary-Layer Flow Control Using Fluidic Oscillators [C] . Tenzin Choephel, James Coder, Mark D. Maughmer AIAA applied aerodynamics conference . 2012
• 7. Wind tunnel testing of an airfoil with a moving surface boundary-layer control. [D] . Al-Garni, Abdullah Mohammed. 1999
• 8. Role of Polymeric Coating on Metallic Foams to Control the Aeroacoustic Noise Reduction of Airfoils with Permeable Trailing Edges [O] . Reza Hedayati, Alejandro Rubio Carpio, Salil Luesutthiviboon, 2019
• 9. Wind tunnel testing of an airfoil with a moving surface boundary-layer control. [O] . Al-Garni Abdullah Mohammed 1999
• 10. Wind-tunnel investigation of boundary-layer control by suction on the NACA 653-418, a = 1.0 airfoil section with a 0.29-airfoil-chord double slotted flap [R] . Quinn, John H , Jr 1946

• 1. 基于风力机翼型的风洞侧壁边界层控制实验研究 [C] . 张传侠 ,惠增宏 . 中国空气动力学会测控技术专委会第六届三次学术交流会 . 2012
• 2. 等离子体控制翼型边界层转捩实验研究 [A] . 宋天威 . 2016