Citation: | ZHENG Guoyong, YANG Yiren. Flutter of Airfoil with Structural Nonlinearity in Supersonic and Hypersonic Flow[J]. Journal of Southwest Jiaotong University, 2007, 20(5): 578-582. |
GUPTA K K,VOELKER L S.CFD-based aeroelastic analysis of the X-43 hypersonic flight vehicle.AIAA Paper 01-0712,2001.[2] NYDICK I,FRIENDMANN P P,ZHONG X L.Hypersonic panel flutter studies on curved panels.AIAA Paper 95-1485,1995.[3] CHEN R R,BLOSSER M L.Metallic thermal projection system panel flutter study.AIAA Paper 02-0501,2002.[4] 杨翊仁,刘菲.结构非线性二元翼外挂系统气弹复杂反应[J].西南交通大学学报,2006,41(1):7-10.YANG Yiren,LIU Fei.Complex response of an airfoil-store system with structural nonlinearity[J].Journal of Southwest Jiaotong University.2006,41 (1):7-10.[5] 杨翊仁.对称分段线性振子的次谐分叉分析[J].西南交通大学学报,1992,27(6):76-82.YANG Yiren.Subharmonic bifurcation analysis of a periodically forced symmetric piecewise linear oscillator[J].Journal of Southwest Jiaotong University,1992,27 (6):76-82.[6] 刘菲,杨翊仁.立方非线性机翼的二重半稳定极限环分叉[J].西南交通大学学报,2004,39(5):638-640.LIU Fei,YANG Yiren.Bifurcations of 2-multiple semistable limit cycle of airfoils with cubic nonlinearity[J].Journal of Southwest Jiaotong University.2004,39 (5):638-640.[7] 陈桂彬,邹丛青.杨超.等.气动弹性设计基础[M].北京:北京航空航天大学出版社,2004:70-72.[8] 舒仲周,张继业,曹登庆.运动稳定性[M].北京:中国铁道出版社,2001:219-223.[9] 王海期.非线性振动[M].北京:高等教育出版社,1992:90-94.
|