Aircraft having rotative sustaining blades or wings

• 1. 一种适用于具有阶梯式桨榖的重载型旋转机翼飞机的旋翼控制系统 [P] . 中国专利： CN111470039A . 2020-07-31
• 2. 具有断面为双结点椭圆环支撑叶片的旋转软轴支撑管 [P] . 中国专利： CN101699083B . 2011.04.06
• 3. Sustaining blade for rotating wing aircraft [P] . 英国专利： GB623322A . 1949-05-16

  机译： 旋翼飞机的支撑叶片

• 4. Aircraft having rotative sustaining wings or blades [P] . 美国专利： US2252544A . 1941-08-12

  机译： 具有旋转支撑翼或叶片的飞机

• 5. Aircraft with rotative sustaining blades or wings [P] . 美国专利： US1894418A . 1933-01-17

  机译： 带有旋转支撑叶片或机翼的飞机

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• 2. Retarded Harrier Maneuver as a New and Efficient Approach for Fixed-Wing Aircraft to Achieve S/VTOL [J] . Chung-Kiak Poh, Chung-How Poh 航空科学与技术（英文） . 2021,第002期
• 3. Numerical simulations of gas-particle flow behavior created by low-level rotary-winged aircraft flight over particle bed [J] . Xiaoxue JIANG, Yingqiao XU, Chuang WANG, 应用数学和力学（英文版） . 2019,第003期
• 4. Analysis of the effects of blade pitch on the radar return signal from rotating aircraft blades [C] . Martin, J., Mulgrew, . 1992
• 5. Methods for Expanding Rotary Wing Aircraft Health and Usage Monitoring Systems to the Rotating Frame through Real-time Rotor Blade Kinematics Estimation. [D] . Allred, Charles Jefferson. 2015
• 6. A report – recommended standards for UK fixed wing medical air transport systems and for patient management during transfer by fixed wing aircraft [O] . A Bristow, N J Toff 1992
• 7. DESIGN FABRICATION OF TWO SEATED AIRCRAFT WITH AN ADVANCED ROTATING LEADING EDGE WING [O] . 100
• 8. Aerodynamics of rotating-wing aircraft with blade-pitch control [R] . Pfluger, A 1940

• 1. Parametric CAD Modelling of Aircraft Wings for FEA Vibration Analysis [J] . Shengyong Zhang ,Mike Mikulich . 应用数学与应用物理（英文） . 2021,第5期
• 2. Experimental investigation of lift enhancement for flying wing aircraft using nanosecond DBD plasma actuators [J] . 姚军锴 ,周丹杰 ,何海波 . 等离子体科学与技术：英文版 . 2017,第4期
• 3. 具有极性判别功能的旋转叶片式静电电位计的研制 [C] . 张雷 ,郎殿永 ,王士海 . 中国物理学会第八届静电学术年会 . 1999
• 4. 鸭式旋转机翼飞机空气动力学关键问题研究 [A] . 孙威 . 2016