[83]张强, 祝小平, 周洲, 等. 高空长航时飞翼布局无人机静气动弹性研究[J]. 飞行力学, 2016, 34(1): 40

ZHANG Qiang, ZHU Xiaoping, ZHOU Zhou, et al. Study on static aeroelasticity of high altitude long endurance flying wing UAV[J]. Flight Dynamics, 2016, 34(1): 40. DOI: 10.13645/j.cnki.f.d.20150918.001

[84]刘湘宁, 向锦武. 大展弦比复合材料机翼的非线性颤振分析[J]. 航空学报, 2006, 27(2): 213

LIU Xiangning, XIANG Jinwu. Study of nonlinear flutter of high-aspect-ratio composite wing[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(2): 213. DOI: 10.3321/j.issn:1000-6893.200602.009

[85]ATTARAN A, MAJID D L, BASRI S, et al. Structural optimization of an aeroelastically tailored composite flat plate made of woven fiberglass/epoxy[J]. Aerospace Science and Technology, 2011, 15(5): 393. DOI: 10.1016/j.ast.2010.09.005

[86]KAMEYAMA M, FUKUNAGA H. Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters[J]. Computers and Structures, 2007, 85(3/4): 213. DOI: 10.1016/j.compstruc.2006.08.051

[87]CESNIK C E S, BROWN E L. Modeling of high aspect ratio active flexible wings for roll control[C]//Proceedings of the 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Denver, Colored: AIAA, 2002: 1. DOI: 10.2514/6.2002-1719

[88]CESNIK C E S, BROWN E L. Active warping control of a joined wing-tail airplane configuration[C]//Proceedings of the 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Norfolk, Virginia: AIAA, 2003: 1. DOI: 10.2514/6.2003-1715

[89]BROWN E L. Integrated strain actuation in aircraft with highly flexible composite wings[D]. Cambridge: Massachusetts Institute of Technology, 2003

[90]SU Weihua, CESNIK C E S. Dynamic response of highly flexible flying wings[J]. AIAA Journal, 2011, 49(2): 324. DOI: 10.2514/1.J050496

[91]SU Weihua, CESNIK C E S. Nonlinear aeroelasticity of a very flexible blended-wing-body aircraft[J]. Journal of Aircraft, 2010, 47(5): 1539. DOI: 10.2514/1.47317

[92]TANG D, GRASCH A, DOWELL E H. Gust response forflexibly suspended high-aspect ratio wings[J]. AIAA Journal, 2010, 48(10): 2430. DOI: 10.2514/1.J050309

[93]PATIL M J, HODGES D H, CESNIK C E S. Nonlinear aeroelastic analysis of complete aircraft in subsonic flow[J]. Journal of Aircraft, 2000, 37(5): 753. DOI: 10.2514/2.2685

[94]PATIL M J. Limit cycle oscillations of aircraft due to flutter-induced drag[C]//Proceedings of the 43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Denver, Colorado: AIAA, 2002: 1. DOI: 10. 2514/6.2002-1409

[95]PATIL M J, HODGES D H. Output feedback control of nonlinear aeroelastic response of a slender wing[J]. Journal of Guidance Control and Dynamics, 2002, 25(2): 302. DOI: 10.2514/2.4882

[96]KIM K, STRGANAC T W. Nonlinear responses of a cantilever wing with an external store[C]//Proceedings of the 44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference. Norfolk, Virginia: AIAA, 2003: 1. DOI: 10.2514/6.2003-1708

[97]ZHANG Jian, XIANG Jinwu. Nonlinear aeroelastic response of high-aspect-ratio flexible wings[J]. Acta Aeronautica et Astronautica Sinica, 2009(4): 355. DOI: 10.1016/s1000-9361(08)60111-9

[98]向锦武, 李道春, 赵仕伟. 一种考虑气动弹性约束的复合材料机翼多目标优化设计方法: 201310607041.2[P]. 2014-03-19

[99]向锦武, 李道春, 赵仕伟, 等. 一种基于气动力降阶模型的复合材料机翼优化设计方法: 201810145057.9[P]. 2018-02-12

[100]GUO Shijun, LI Daochun, LIU Y.Multi-objective optimization of a composite wing subject to strength and aeroelastic constraints[J]. Proceedings of the Institution of Mechanical Engineers, Part G Journal of Aerospace Engineering, 2012, 226(9): 1095. DOI: 10.1177 /09544100114177

[101]万志强, 杨超. 大展弦比复合材料机翼气动弹性优化[J]. 复合材料学报, 2005, 22(3): 145

WAN Zhiqiang, YANG Chao. Aeroelastic optimization of a high aspect ratio composite wing[J]. Acta Materiae Compositae Sinica, 2005, 22(3): 145. DOI: 10.3321/j.issn:1000-3851.2005.03.028

[102]白俊强, 辛亮, 刘艳, 等. 复合材料后掠机翼的气动弹性剪裁方法研究[J]. 西北工业大学学报, 2014, 32(6): 843

BAI Junqiang, XIN Liang, LIU Yan, et al. Exploring anaeroelastic tailoring design method for composite backswept wing[J]. Journal of Northwestern Polytechnical University, 2014, 32(6): 843. DOI:10.3969/j.issn.1000-2758.2014. 06.001