[103]刘湘宁, 向锦武. 大展弦比柔性复合材料机翼的气动弹性剪裁[J]. 北京航空航天大学学报, 2006, 32(12): 1403
LIU Xiangning, XIANG Jinwu. Study of aeroelastic tailoring of high-aspect-ratio flexible composite wing[J]. Journal of Beijing University of Aeronautics and Astronautics,2006, 32(12): 1403. DOI: 10.3969/j.issn.1001-5965.2006.12.003
[104]向锦武, 张雪娇, 赵仕伟, 等. 大展弦比复合材料机翼研究进展[J]. 哈尔滨工业大学学报, 2017, 49(10): 1
XIANG Jinwu, ZHANG Xuejiao, ZHAO Shiwei, et al. Recent advance in high-aspect-ratio composite wing[J]. Journal of Harbin Institute of Technology, 2017, 49(10): 1. DOI: 10.11918/j.issn.0367-6234.201705036
[105]张纪奎, 郦正能, 寇长河. 大展弦比复合材料机翼结构设计研究[J]. 航空学报, 2005, 26(4): 450
ZHANG Jikui, LI Zhengneng, KOU Changhe. Structural design of high aspect ratio composite material wing[J]. Acta Aeronautica et Astronautica Sinica, 2005, 26(4): 450. DOI: 10.3321/j.issn:1000-6893.2005.04.014
[106]刘峰, 马佳, 张春, 等. 某无人机复合材料主翼盒准等强度设计与有限元分析[J]. 玻璃钢/复合材料, 2015(4): 16
LIU Feng, MA Jia, ZHANG Chun, et al. Quasi-equal strength design and finite element analysis for composite main wing box of X UAV[J]. Fiber Reinforced Plastics/Composites, 2015(4): 16. DOI: 10.3969/j.issn.1003-0999.2015.04.003
[107]杨龙. 大展弦比太阳能无人机结构动力学研究[D]. 长沙: 国防科学技术大学, 2013
YANG Long. Research on structural dynamics of solar energy unmanned aerial vehicle[D]. Changsha: National University of Defense Science and Technology, 2013
[108]MEDDAIKAR Y M, DILLINGER J K S, SODJA J, et al. Optimization, manufacturing and testing of a composite wing with maximized tip deflection[C]//Proceedings of the 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. San Diego, California: AIAA Scitech Forum, 2016: 1. DOI: 10.2514/6.2016-0489
[109]VIO G A, COOPER J E. Optimization of the composite sensorcraft structure for gust alleviation[C]//Proceedings of the 12th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. Victoria, British Columbia, Canada: AIAA, 2008: 1. DOI: 10.2514/6.2008-6017
[110]GAUTHIER-PERRON S, DRELA M. Passive gust load alleviation through bend-twist coupling of composite beams on typical commercial airplane wings[C]//Proceedings of the 54th AIAA/ASME/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Boston, Massachusetts: AIAA, 2013: 1. DOI: 10. 2514/6.2013-1490
[111]PARK W S, SHIN W J, KIM T. Development of the main wing structure of a high altitude long endurance UAV[J]. International Journal of Aeronautical & Space Sciences, 2018, 19(1): 53. DOI: 10.1007/s42405-018-0002-x
[112]《飞机设计手册》总编委会. 飞机设计手册第9册: 载荷、强度和刚度[M]. 北京: 航空工业出版社, 2001
Aircraft Design Manual’s Editors. Aircraft design manual 9: load, strength and stiffness[M]. Beijing: Aviation Industry Press, 2001
[113]汤平. 两种民用飞机翼身对接结构比较分析[J].航空制造技术, 2018, 61(13): 28
TANG Ping. Comparison and analysis on outer wing-fuselage connection of two civil aircrafts[J]. Aeronautical Manufacturing Technology. 2018, 61(13): 28.DOI: 10.16080/j.issn1671-833x.2018.13.028
[114]BENJAMIN J, SAM C, DANIEL C, et al. Digital morphing wing active wing shaping concept using composite lattice-based cellular structures[J]. Soft Robotics, 2017, 4(1): 33. DOI: 10.1089/soro.2016.0032
[115]胡江波, 梁宪珠, 张铖, 等. 高载荷质量比复合材料机翼模型结构设计与制造研究[J]. 材料开发与应用, 2011, 26(3): 41
HU Jiangbo, LIANG Xianzhu, ZHANG Cheng, et al. Study on structure design and manufacture of high load-weight ratio composite wing model[J]. Development and Application of Materials, 2011, 26(3): 41. DOI: 10.19515/j.cnki.1003-1545.2011.03.011
[116]向锦武, 李道春, 赵仕伟, 等. 一种复合材料机翼防固化变形模具设计: 201810151683.9[P]. 2018-08-31
[117]向锦武, 李道春, 张雪娇, 等. 一种复合材料机翼开口补强的优化设计方法: 201810146327.8[P]. 2018-09-04
[118]张健. 柔性飞机非线性气动弹性与飞行动力学耦合建模与仿真[D]. 北京:北京航空航天大学, 2010
ZHANG Jian. Modeling and simulation of coupled nonlinear aeroelasticity and flight dynamics for flexible aircraft[D].Beijing: Beihang University, 2010
[119]WASZAK M R, SCHMIDT D K. Flight dynamics of aeroelastic vehicles[J]. Journal of Aircraft, 1988, 25(6): 563. DOI: 10.2514/3.45623
[120]BUTTRILL C S, ARBUCKLE P D, ZEILER T A. Nonlinear simulation of a flexible aircraft in maneuvering flight[C]//Proceedings of the AIAA Flight Simulation Technologies Conference. Monterey, CA: AIAA, 1987: 122. DOI: 10.2514/6.1987-2501