[40]王鑫, 李山, 唐湛棋, 等. 沟槽对湍流边界层中展向涡影响的实验研究[J]. 实验流体力学, 2018, 32(1): 55
WANG Xin, LI Shan, TANG Zhanqi, et al. An experimental study on riblet-induced spanwise vortices in turbulent boundary layers[J]. Journal of Experiments in Fluid Mechanics, 2018, 32(1): 55. DOI: 10.11729/syltlx20170092
[41]CHANDRASEKHARA M S, MARTIN P B, TUNG C. Compressible dynamic stall control using a variable droop leading edge airfoil[J]. Journal of Aircraft, 2004, 41(4): 862. DOI: 10.2514/1.472
[42]JEFFREY D, ZHANG Xin, HURST D W. Aerodynamics of Gurney flaps on a single-element high-lift wing[J]. Journal of Aircraft, 2000, 37(2): 295. DOI: 10.2514/2.2593
[43]LI Daochun, ZHAO Shiwei, ANDREA D R, et al. A review of modelling and analysis of morphing wings[J]. Progress in Aerospace Sciences, 2018, 100: 46. DOI: 10.1016/j.paerosci.2018.06.002
[44]MONNER H P. Realization of an optimized wing camber by using form variable flap structures[J]. Aerospace Science and Technology, 2001, 5(7): 445. DOI: 10.1016/s1270-9638(01)01118-x
[45]LAFOUNTAIN C, COHEN K, ABDALLAH S. Camber controlled airfoil design for morphing UAV[C]//Proceedings of the 47th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Orlando, Florida: AIAA, 2009: 092407. DOI: 10.2514/6.2009-1435
[46]DELLA V P, CORCIONE S, PECORA R, et al. Design and integration sensitivity of a morphing trailing edge on a reference airfoil: The effect on high-altitude long-endurance aircraft performance[J]. Journal of Intelligent Material Systems and Structures, 2017, 28(20): 2933. DOI: 10.1177/1045389X17704521
[47]NANGIA R K, PALMER M E, TILMANN C. Planform variation effects, unconventional high aspect-ratiojoined-wing aircraft incorporating laminar-flow[C]//Proceedings of the 43rd AIAA Aerospace Sciences Meeting and Exhibit. Reno, Nevada: AIAA, 2005: 1. DOI: 10.2514/6.2005-243
[48]李军, 李占科, 宋笔锋. 联翼高空长航时无人机总体布局设计研究[J]. 飞行力学, 2009, 27(4): 1
LI Jun, LI Zhanke, SONG Bifeng. Conceptual layout design of the joined-wing High-Altitude-Long-Endurance UAV[J]. Flight Dynamics, 2009, 27(4): 1. DOI: 10.13645/j.cnki.f.d.2009.04.001
