| Citation: | YIN Lei-lei, ZHANG Si-jin, WEN Gui-lin, XU Hui-dong. Analysis on the system bifurcation and coexistence of multiple solutions for typical airfoil section with freeplay[J]. Journal of Aerospace Power, 2014, (6): 1410-1416. doi: 10.13224/j.cnki.jasp.2014.06.022 |
| [1] |
Ashley H,Zartarian G.Piston theory:a new aerodynamic tool for the aeroelastician[J].Journal of Aeronaut Science,1956,23(12):1109-1118.
|
| [2] |
Liviu L,Gianfranco C,Picrgiovanni M.Implications of cubic physical/aerodynamic non-linearities on the character of the flutter instability boundary[J].International Journal of Non-Linear Mechanics,2003,38:173-199.
|
| [3] |
Sander G,Bon C,Geradin M.Finite element analysis of supersonic panel flutter[J].International Journal for Numerical Methods in Engineering,1973,7(3):379-394.
|
| [4] |
Mcintosh J R S C,Reed J R R E,Rodden W P.Experimental and theoretical study of nonlinear flutter[J].Journal of Aircraft,1981,18(12):1057-1063.
|
| [5] |
Sheta E F,Harrand V J,Thompson D E,et al.Computational and experimental investigation of limit cycle oscillations of nonlinear aeroelastic systems[J].Journal of Aircraft,2002,39(1):133-141.
|
| [6] |
Liu L,Wong Y S,Lee B H K.Application of the center manifold theory in nonlinear aeroelasticity[J].Journal of Sound and Vibration,2000,234(4):641-659.
|
| [7] |
Sadaghat A,Copper J E.Limit cycle oscillation prediction for aeroelastic systems with continuous nonlinearities[J].AIAA 2000-1397,2000.
|
| [8] |
郑国勇,杨翊仁.结构非线性机翼的超音速和高超音速颤振[J].西南交通大学学报,2007,42(5):578-582. ZHENG Guoyong,YANG Yiren.Flutter of airfoil with structural nonlinearity in supersonic and hypersonic flow[J].Journal of Southwest Jiaotong University,2007,42(5):578-582.(in Chinese)
|
| [9] |
王益峰,邵松,朱清华,等.带有气动及结构非线性的二元机翼颤振分析[J].航空动力学报,2012,27(9):2063-2074. WANG Yifeng,SHAO Song,ZHU Qinghua,et al.Flutter analysis of a two-dimensional wing with aerodynamic and structural non-linearity[J].Journal of Aerospace Power,2012,27(9):2063-2074.(in Chinese)
|
| [10] |
Bunton R W,Denegri J R C M.Limit cycle oscillation characteristics of fighter aircraft[J].Journal of Aircraft,2000,37(5):916-918.
|
| [11] |
Denegri J R C M.Limit cycle oscillation test results of a fighter with external stores[J].Journal of Aircraft,2000,37(5):761-769.
|
| [12] |
Ding Q,Wang L D.Flutter control of a two-dimensional airfoil using wash-out filter technique[J].Chinese Journal of Aeronautics,2005,18(2):130-136.
|
| [13] |
于明礼,文浩,胡海岩,等.二维翼段颤振的μ控制[J].航空学报,2007,28(2):340-343. YU Mingli,WEN Hao,HU Haiyan,et al.Active flutter suppression of a two-dimensional airfoil section using μ synthesis[J].Acta Aeronautica et Astronautica Sinica,2007,28(2):340-343.(in Chinese)
|
| [14] |
李道春,向锦武.间隙非线性气动弹性颤振控制[J].北京航空航天大学学报,2007,33(6):640-643. LI Daochun,XIANG Jinwu.Flutter control of aeroelasticity with freeplay nonlinearity[J].Journal of Beijing University of Aeronautics and Astronautics,2007,33(6):640-643.(in Chinese)
|
| [15] |
任爱娣,张琪昌.具有不对称间隙的二元机翼颤振研究[J].工程力学,2006,23(9):25-29. REN Aidi,ZHANG Qichang.The flutter study of a two-dimensional airfoil with asymmetry freeplay[J].Engineering Mechanics,2006,23(9):25-29.(in Chinese)
|
| [16] |
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[J].航空学报,2003,24(6):521-525. ZHAO Yonghui,HU Haiyan.Aeroelastic analysis of a two-dimensional airfoil with control surface freeplay nonlinearity[J].Acta Aeronautica et Astronautica Sinica,2003,24(6):521-525.(in Chinese)
|
| [17] |
Zhang S J,Wen G L,Peng F,et al.Analysis to limit cycle vibration of a typical airfoil section with freeplay[J].Acta Mechanica Sinica,2013,29(4):583-592.
|