| 专著：赵永辉，《气动弹性力学与控制》，科学出版社，2007.8 论文： 1. Zhao Y H， Aeroelastic stability of a two-dimensional airfoil with time-delayed feedback control， Journal of Fluid and Structures(submittied) 2. Zhao Y H, Hu H Y, Aeroelastic analysis of a non-linear airfoil based on unsteady vortex lattice model, Journal of Sound and Vibration, 2004, 276:491-510 3. Zhao Y H, Sun W, Hu H Y, Flutter suppression of Aircraft control surface with MR damper, Proceedings of the 5th international conference on vibration engineering, 2002 5. Zhao Y H, Hu H Y. Structural modeling and aeroelastic analysis of a high-aspect-ratio composite wing. Chinese Journal of Aeronautics, 2005,18(1):25-30 6. 赵永辉,胡海岩, 具有操纵面间隙非线性二维翼段的气动弹性分析, 航空学报, 2003, 24(6):521-525 7. 赵永辉, 胡海岩, 大展弦比夹芯翼大攻角颤振分析, 振动工程学报, 2004, 17(1):25-29 8. 赵永辉, 胡海岩, 一类非线性系统的滑模振动主动控制, 南京航空航天大学学报, 2003, 35(3):308-312 专著：赵永辉，《气动弹性力学与控制》，科学出版社，2007.8 论文： 1. Zhao Y H， Aeroelastic stability of a two-dimensional airfoil with time-delayed feedback control， Journal of Fluid and Structures(submittied) 2. Zhao Y H, Hu H Y, Aeroelastic analysis of a non-linear airfoil based on unsteady vortex lattice model, Journal of Sound and Vibration, 2004, 276:491-510 3. Zhao Y H, Sun W, Hu H Y, Flutter suppression of Aircraft control surface with MR damper, Proceedings of the 5th international conference on vibration engineering, 2002 5. Zhao Y H, Hu H Y. Structural modeling and aeroelastic analysis of a high-aspect-ratio composite wing. Chinese Journal of Aeronautics, 2005,18(1):25-30 6. 赵永辉,胡海岩, 具有操纵面间隙非线性二维翼段的气动弹性分析, 航空学报, 2003, 24(6):521-525 7. 赵永辉, 胡海岩, 大展弦比夹芯翼大攻角颤振分析, 振动工程学报, 2004, 17(1):25-29 8. 赵永辉, 胡海岩, 一类非线性系统的滑模振动主动控制, 南京航空航天大学学报, 2003, 35(3):308-312 |
