| [1] Benedict M, Ramasamy M, Chorpra I, et al. Performance of a cycloidal rotor concept for micro-air-vehicle applications[J]. Journal of the American Helicopter Society, 2010, 55(2): 1-14.[2] Hu Y, Lim K B, Hu W R. The research on the performance of cyclogyro, AIAA-2006-7704. Reston: AIAA, 2006.[3] Jarugumilli T, Benedict M, Chopra I. Experimental optimization and performance analysis of a MAV scale cycloidal rotor, AIAA-2011-0821. Reston: AIAA, 2011.[4] Iosilevskii G, Levy Y. Experimental and numerical study of cyclogiro aerodynamics[J]. AIAA Journal,2006, 44(12): 2866-2870.[5] Benedict M, Jarugumilli T. Experimental and computational studies to understand the role of flow curvature effects on the aerodynamic performance of a MAV-scale cycloidal rotor in forward flight, AIAA-2012-1629. Reston: AIAA, 2012.[6] Shrestha E, Benedict M, Chopra I. Autonomous hover capability of cycloidal-rotor micro air vehiclem, AIAA-2013-0121. Reston: AIAA, 2013.[7] Mcnabb M L. Development of a cycloidal propulsion computer model and comparison with experiment. Mississippi: Mississippi State University, 2001.[8] Adams Z, Fagley C. Novel cyclorotor pitching mechanism for operation at curtate and prolate advance ratios, AIAA-2013-0501. Reston: AIAA, 2013.[9] Benedict M, Ramasamy M, Chopra I, et al. Experiments on the optimization of the MAV-scale cycloidal rotor characteristics towards improving their aerodynamic performance//Proceedings of the International Specialists' Meeting on Unmanned Rotorcraft. Scottsdale: Curran Associates, 2009: 545-546[10] Benedict M, Jarugumilli T, Chopra I. Experimental performance optimization of a MAV-scale cycloidal rotor//Proceedings of the AHS Specialists' Meetings on Aerodynamics. San Francisco: Curran Associates, 2010: 20-22.[11] Benedict M, Jarugumilli T, Chopra I. Design and development of a hover-capable cyclocopter MAV//Proceedings of the 65th Annual National Froum of the American Helicopter Society. Grapevine: Curran Associates, 2009: 27-29.[12] Parsons E. Investigation and characterization of a cycloidal rotor for application to a micro air vehicle. Maryland: University of Maryland, 2005.[13] Sirohi J, Parsons E, Chopra I. Hover performance of a cycloidal rotor for a micro air vehicle[J]. Journal of the American Helicopter Society, 2007, 52(3): 263-279.[14] Hwang I S, Min S Y, Lee C H, et al. Development of a four-rotor cyclocopter[J]. Journal of Aircraft, 2008, 45(6): 25-48.[15] Fagley C, Porter C, McLaughlin T. Curvature effects of a cycloidally rotating airfoil, AIAA-2014-0255. Reston: AIAA, 2014.[16] Kim S J, Yun C Y, Kim D, et al. Design and performance tests of cycloidal propulsion systems, AIAA-2003-1786. Reston: AIAA, 2003.[17] Nozaki H, Sekiguchi Y, Matsuuchi K. Research and development on cycloidal propellers for airships, AIAA-2009-2850. Reston: AIAA, 2009.[18] Matsuuchi K, Ohtsuka N, Kimura Y. Cycloidal propeller and its application to advanced LTA to advanced LTA vehicles, AIAA-2003-0683. Reston: AIAA, 2003.[19] Iosilevskii G, Levy Y. Aerodynamics of the cyclogiro, AIAA-2003-3473. Reston: AIAA, 2003.[20] Hu Y, Tay W B,Lim K B. The analysis of cyclogyro using unsteady vortex lattice method//Proceedings of 25th Congress of the International Council of the Aeronautical Sciences. Hamburg: Curran Associates, 2006: 930-935.[21] Jameson A. An assessment of dual-time stepping, time spectral and artificial compressibility based numerical algorithms for unsteady flow with applications to flapping wings, AIAA-2009-4273. Reston: AIAA, 2009[22] Liu Z, Yang Y J, Zhou W J, et al. Study of unsteady separation flow of around airfoil at high angle of attack using hybrid RANS-LES method[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(2): 372-380. (in Chinese) 刘周, 杨云军, 周伟江, 等. 基于RANS-LES混合方法的翼型大迎角非定常分离流动研究[J]. 航空学报, 2014, 35(2): 372-380.[23] Yang J G, Wu H. Explicit coupled solution of two-equation k-ω SST turbulence model and its application in turbomachinery flow simulation[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(1): 116-124. (in Chinese) 杨金广, 吴虎.双方程k-ω SST湍流模型的显示耦合求解及其在叶轮机械中的应用[J]. 航空学报, 2014, 35(1): 116-124.[24] Yang Y, Li D, Zhang Z H. Influence of flapping wing micro aerial vehicle unsteady motion on horizontal tail[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(10): 1827-1833. (in Chinese) 杨茵, 李栋, 张振辉.微型扑翼飞行器非定常运动对平尾的影响[J]. 航空学报, 2012, 33(10): 1827-1833. |
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