Side force control on slender body by self-excited oscillation flag
Tài liệu tham khảo
Wang, 2007, Evolution mechanism for wake-type flow over slender body, Eng. Mech., 24, 25
Cai, 2011, Design of optimal wing-body configuration to delay onset of vortex asymmetry, AIAA J., 49, 164, 10.2514/1.J050595
Ma, 2008, Tip-disturbance effects on asymmetric vortex breakdown around a chined forebody, J. Aircr., 45, 1098, 10.2514/1.31352
Bernhardt, 1998, Proportional control of asymmetric forebody vortices, AIAA J., 36, 2087, 10.2514/2.310
Liu, 2008, Flow control over a conical forebody using duty-period plasma actuators, AIAA J., 46, 2969, 10.2514/1.39435
Ming, 2005, Flow control and mechanism for slender body at high angle of attack, Modern Phys. Lett. B, 19, 1571, 10.1142/S0217984905009936
G. Malcolm, Forebody vortex control: a progress review, AIAA Paper 93-3540, Aug. 1993.
Ma, 2007, Effects of forced asymmetric transition on vortex asymmetry around slender bodies, AIAA J., 45, 2671, 10.2514/1.29712
Zhang, 2012, Experimental study on side force alleviation of conical forebody with a fluttering flag, Phys. Fluids, 24, 124105, 10.1063/1.4772201
Zhai, 2014, Side force control on slender body by vortex generators, Chin. J. Theor. Appl. Mech., 46, 308
Modi, 1984, Aerodynamics of pointed forebodies at high angles of attack, J. Aircr., 21, 428, 10.2514/3.44983