Effects of free stream local disturbance on delta wing aerodynamics

[1] Taylor G, Kroker A, Gursul I. Passive flow control over flexible non-slender delta wings . AIAA-2005-0865, 2005 [2] 伍康.弹性对40°后掠切尖三角翼气动特性的影响 .北京:北京航空航天大学航空科学与工程学院,2005 Wu Kang.The effect of flexibility on aerodynamics of 40-deg sweep cropped delta wings . Beijing: School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, 2005(in Chinese) [3] Gordiner R E, Visbal M R. Computation of the aeroelastic response of a flexible delta wing at high angles of attack . AIAA-2003-1728, 2003 [4] Ifju P G, Jenkins D A, Ettinger S, et al. Flexible wing based micro air vehicles . AIAA-2002-0705, 2002 [5] 王晋军,伍康.机翼弹性变形对气动特性影响的实验研究[J].空气动力学学报,2007,25(1):55-59 Wang Jinjun,Wu Kang.Experimental investigations of the effect of wing elastic deformations[J]. Acta Aerodynamica Sinica, 2007,25(1):55-59(in Chinese) [6] Spedding G R, Lissaman P B S. Technical aspects of microscale flight systems[J]. Journal of Avian Biology, 1998, 29(4):458-468 [7] Heron I, Myose R Y. Impingement of a von karman vortex street on a delta wing[J]. Journal of Aircraft, 2005, 42(4):1084-1087 [8] Muller T J, Delaurier J D. Aerodynamics of small vehicles[J]. Annual Review of Fluid Mechanics, 2003, 35(1):89-111 [9] Rediniotis O K, Stapountzis H, Telionist D P. Periodic vortex shedding over delta wings[J]. AIAA Journal, 1993, 31(9):1555-1562