Citation: | YE Xianhui, YANG Yiren. Flutter of Delta Wing under Aerodynamic Heating[J]. Journal of Southwest Jiaotong University, 2008, 21(1): 62-66. |
叶献辉,杨翊仁,刘菲.非对称结构参数对颤振速度的影响[J].西南交通大学学报,2005,40(6):779-782.YE Xianhui,YANG Yiren,LIU Fei.Effects of asymmetrical parameters of structure on structural flutter velocity[J].Journal of Southwest Jiaotong University,2005,40(6):779-782.[2] COLE S R,FLORANCE J R,THOMASON L B.Supersonic aeroelastic instability results for a NASP like wing model[C]//34th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.La Jolla:[s.n.] ,1993:638-647.[3] HEEG J,ZEILER T,POTOTZKY A.Aerothermoelastic Analysis of a NASP Demonstrator Model[C]//34th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference.La Jolla:[s.n.] ,1993:617-627.[4] 张伟伟.超音速、高超音速非线性气动弹性问题研究[D].硕士学位论文.西安:西北工业大学,2004.[5] MCNAMARA J,FRIEDMANN P,POWELK,et al.Three-dimensional deroelastic and aerothermoelastic behavior in hypersonic flow[C]// 46th AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conference,Austin:[s.n.] ,2005:4655-4701.[6] 吴志刚,惠俊鹏,杨超.高超声速下翼面的热颤振工程分析[J].北京航空航天大学学报,2005,31(3):270-273.WU Zhigang,HUI Junpeng,YANG Chao.Hypersonic aerothermoelastic analysis of wings[J].Journal of Beijing University of Aeronautics and Astronautics,2005,31 (3):270-273.[7] RODDEN W P,JOHNSON E H.MSC/NASTRAN aeroelastic analysis users guide[M].Santa Ana:MSC.Software Corporation,2002:337-492.[8] 车竞,唐硕,何开锋.类乘波体飞行器气动加热的工程计算方法[J].弹道学报,2006,18(4):93-96.CHE Jing,TANG Shuo,HE Kaifeng.Engineering calculation of aerodynamic heating for quasi-waverider vehicle[J].Journal of Ballistics,2006,18(4):93-96.[9] 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.[10] 钱翼稷.空气动力学[M].北京:北京航空航天大学出版社,2004:94-104.
|