Supersonic Panel Flutter Analysis of Delaminated Plates
暂无分享,去创建一个
Masaki Kameyama | Hisao Fukunaga | Ning Hu | Tatsuya Hanawa | N. Hu | H. Fukunaga | M. Kameyama | T. Hanawa
[1] Maher N. Bismarck-Nasr,et al. Finite Element Analysis of Aeroelasticity of Plates and Shells , 1992 .
[2] Chih-Chen Chang,et al. Finite element supersonic flutter analysis of skewed and cracked composite panels , 1998 .
[3] Michel Géradin,et al. Finite element analysis of Supersonic panel flutter , 1973 .
[4] Ning Hu,et al. LOW-VELOCITY IMPACT RESPONSE OF COMPOSITE LAMINATES WITH A DELAMINATION , 1998 .
[5] Victor Y. Perel,et al. Finite Element Analysis of Vibration of Delaminated Composite Beam with an Account of Contact of the Delamination Crack Faces, Based on the First-order Shear Deformation Theory , 2005 .
[6] Ramana M. Pidaparti,et al. Free vibration and flutter of damaged composite panels , 1997 .
[7] Aditi Chattopadhyay,et al. Aeroelastic control of smart composite plate with delaminations , 2000 .
[8] P. M. Mujumdar,et al. Flexural vibrations of beams with delaminations , 1988 .
[9] E. Dowell. Panel flutter - A review of the aeroelastic stability of plates and shells , 1970 .
[10] Serge Abrate,et al. Impact on Composite Structures , 1998 .
[11] T. A. Weisshaar,et al. Panel flutter suppression using adaptive material actuators , 1994 .
[12] Masaki Kameyama,et al. Vibration analysis of delaminated composite beams and plates using a higher-order finite element , 2002 .
[13] Ning Hu,et al. Buckling analysis of delaminated laminates with consideration of contact in buckling mode , 1999 .
[14] Y. Y. Liu,et al. Vibrations of split beams , 1982 .
[15] Holt Ashley,et al. Piston Theory-A New Aerodynamic Tool for the Aeroelastician , 1956 .
[16] Hisao Fukunaga,et al. Panel Flutter Design of Symmetrically Laminated Plates Using Lamination Parameters. , 1998 .