[68]STUHLPFARRER M, VALERO-ANDREU A, BREITSAMTER C.Numerical and experimental investigations of the propeller characteristics of an electrically powered ultralight aircraft[J]. CEAS Aeronautical Journal, 2017, 8(3): 441. DOI: 10.1007/s13272-017-0245-4
[69]NICKOL C, GUYUN M, KOHOUT L, et al. High altitude long endurance air vehicle analysis of alternatives and technology requirements development[C]//Proceedings of the 45th AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: AIAA, 2007: 1. DOI: 10.2514/6.2007-1050
[70]FLITTIE K, CURTIN B. Pathfinder solar-powered aircraft flight performance[C]//Proceedings of the 23rd Atmospheric Flight Mechanics Conference. Boston, MA: AIAA, 1998: 618. DOI: 10.2514/6.1998-4446
[71]YOUNGBLOOD J W, TALAY T A. Solar-powered airplane design for long-endurance, high-altitude flight[C]//Proceedings of the 2nd International Very Large Vehicles Conference. Washington, DC: AIAA, 1982: 1. DOI: 10.2514/6.1982-811
[72]张健, 向锦武. 柔性飞机非线性气动弹性与飞行动力学耦合静、动态特性[J]. 航空学报, 2011, 32(9): 1569
ZHANG Jian, XIANG Jinwu. Static and dynamic characteristics of coupled nonlinear aeroelasticity and flight dynamics of flexible aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(9): 1569. DOI: CNKI: 11-1929/V.20110509.1158.006.
[73]李道春, 向锦武. 间隙非线性气动弹性颤振控制[J]. 北京航空航天大学学报, 2007, 33(6): 640
LI Daochun, XIANG Jinwu. Flutter control of aeroelasticity with freeplay nonlinearity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(6): 640
[74]LI Daochun, GUO Shijun, XIANG Jinwu. Aeroelastic dynamic response and control of an airfoil section with control surface nonlinearities[J]. Journal of Sound and Vibration, 2010, 329(22): 4756. DOI: 10.1016/j.jsv.2010.06.006.
[75]PETERS D A, KARUNAMOORTHY S, CAO Wenming.Finite-state induced flow models, Part I: Two-dimensional thin airfoil[J]. Journal of Aircraft, 1995, 32(2): 313. DOI: 10.2514/3.46718
[76]LIU Yi, XIE Changchuan, YANG Chao, et al. Gust response analysis and wind tunnel test for a high-aspect ratio wing[J]. Chinese Journal of Aeronautics, 2016, 29(1): 91. DOI: 10.1016/j.cja.2015.12.013
