Structural component of the fuselage wing for connecting two wings of lift and a section of the fuselage in a plane.

• 1. 用于连接飞机上的两个主机翼和机身段的机翼-机身-结构件 [P] . 中国专利： CN101909989B . 2013.04.10
• 2. 用于连接飞机上的两个主机翼和机身段的机翼-机身-结构件 [P] . 中国专利： CN101909989A . 2010-12-08
• 3. Structural wing-fuselage component for connecting two wings to a fuselage section of an aircraft [P] . 美国专利： US8356773B2 . 2013-01-22

  机译： 用于将两个机翼连接到飞机机身部分的机翼机身结构部件

• 4. Structural Wing-Fuselage Component For Connecting Two Wings To A Fuselage Section Of An Aircraft [P] . 美国专利： US2010301165A1 . 2010-12-02

  机译： 用于将两个机翼连接到飞机机身部分的机翼-机身结构部件

• 5. STRUCTURAL WING-FUSELAGE COMPONENT FOR CONNECTING TWO WINGS TO A FUSELAGE SECTION ON AN AIRCRAFT [P] . CA2711105A1 . 2009-07-09

  机译： 用于在飞机上将两个机翼连接到机身部分的结构机翼-机身组件

• 1. 3D UNSTRUCTURED GRID GENERATION TECH-NOLOGY EULER SOLUTION FOR WING/FUSELAGE COMBINATION [J] . 中国航空学报：英文版 . 1997,第002期
• 2. FUSELAGE　STRUCTURAL　OPTIMIZATION　WITH　MSC／MOD　PRE－PROCESSING　AND　MSC／PAL2　POST－PROCESSING [J] . 南京航空航天大学学报：英文版 . 1994,第002期
• 3. A computational study of the wing-wing and wing-body interactions of a model insect [J] . Xin Yu, Mao Sun 力学学报：英文版 . 2009,第004期
• 4. Erratum to: A computational study of the wing-wing and wing-body interactions of a model insect [J] . Xin Yu, Mao Sun 力学学报：英文版 . 2009,第006期
• 5. Erratum to： A computational study of the wing-wing and wing-body interactions of a model insect [J] . Xin Yu, Mao Sun 力学学报：英文版 . 2009,第006期
• 6. Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 3: Some Applications of Oscillating Lifting Surface Theory to the Flapping Wing [J] . Valentin Adrian Jean BUTOESCU INCAS Bulletin . 2014,第2期
• 7. Failure analysis of the wing-fuselage connector of an agricultural aircraft [J] . Lucjan Witek Engineering failure analysis . 2006,第4期
• 8. Stress and Fatigue Analysis of Modified Wing-Fuselage Connector for Agricultural Aircraft [J] . Lucjan Witek Journal of Aircraft . 2006,第3期
• 9. Aerodynamic Design of Blended Wing-Body and Lifting-Fuselage Aircraft [C] . Thomas A. Reist, David W. Zingg AIAA applied aerodynamics conference;AIAA aviation forum . 2016
• 10. Structural testing of an ultralight UAV composite wing and fuselage. [D] . Simsiriwong, Jutima. 2009
• 11. Application of Dual Focused Ultrasonic Phased Array Transducer in Two Orthogonal Cross-Sections for Inspection of Multi-Layered Composite Components of the Aircraft Fuselage [O] . Renaldas Raišutis, Olgirdas Tumšys 2020
• 12. Aerodynamic Interference between Oscillating Lifting Surfaces and Fuselage. Part 3: Some Applications of Oscillating Lifting Surface Theory to the Flapping Wing [O] . Valentin Adrian Jean BUTOESCU 2014

• 1. 任意机身表面网格生成及机翼-机身相贯线生成 [C] . 孙刚 . 第八届全国计算流体力学会议 . 1996
• 2. 民机机翼机身对接结构多部位损伤可靠性研究 [A] . 蒋军 . 2018