Dynamic Instability Analysis of Multifunctional Composite Structures
暂无分享,去创建一个
B. Rammohan | P. R. Budarapu | D. Harursampath | P. Budarapu | B. Rammohan | Yashwantha Kumar | D. K. Harursampath | K. N. Seetharamu | K. Seetharamu | Y. Kumar
[1] Chung-Li Liao,et al. Flutter analysis of stiffened laminated composite plates and shells in supersonic flow , 1993 .
[2] M. Donadon,et al. Aeroelastic behavior of stiffened composite laminated panel with embedded SMA wire using the hierarchical Rayleigh–Ritz method , 2017 .
[3] Hermann J. Hassig,et al. An Approximate True Damping Solution of the Flutter Equation by Determinant Iteration , 1971 .
[4] Haiyan Hu,et al. Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification , 2016 .
[6] Gianni Bartoli,et al. Experimental study on the flutter-induced motion of two-degree-of-freedom plates , 2017 .
[7] M. A. Kouchakzadeh,et al. Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression , 2017 .
[8] Chuh Mei,et al. Nonlinear Flutter of Cylindrical Panels Under Yawed Supersonic Flow Using Finite Elements , 2005 .
[9] Peretz P. Friedmann,et al. Aeroelastic and Aerothermoelastic Analysis in Hypersonic Flow: Past, Present, and Future , 2011 .
[10] Earl H. Dowell,et al. Nonlinear flutter of curved plates. II , 1970 .
[11] R. C. Zhou,et al. Finite element time domain : modal formulation for nonlinear flutter of composite panels , 1994 .
[12] Quan Wang,et al. An investigation on the aeroelastic flutter characteristics of FG-CNTRC beams in the supersonic flow , 2017 .
[13] Satyajit S. Ghoman,et al. Time Domain Method for Nonlinear Flutter of Curved Panels under Yawed Supersonic Flow at Elevated Temperature , 2009 .
[14] Dinh Tan Hung,et al. Wind tunnel and initial field tests of a micro generator powered by fluid-induced flutter , 2016 .
[15] Earl H. Dowell,et al. Nonlinear flutter of curved plates. , 1969 .
[16] M. M. Mikulas,et al. Static and dynamic effects of eccentric stiffening of plates and cylindrical shells. , 1966 .
[17] Peretz P. Friedmann,et al. Aerothermoelastic and aeroelastic studies of hypersonic vehicles using CFD , 2013 .
[18] David Y. Xue,et al. Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow , 1992 .
[19] R. Pidaparti,et al. Supersonic flutter analysis of composite plates and shells , 1993 .
[20] M. O. Kaya,et al. Dynamic instability of spinning launch vehicles modeled as thin-walled composite beams , 2017 .
[21] Yongdong Cui,et al. Nonlinear aeroelastic analysis of curved laminated composite panels , 2017 .
[22] Hai Zhao,et al. A study on the aero-elastic flutter of stiffened laminated composite panel in the supersonic flow , 2013 .
[23] Randall J. Allemang,et al. THE MODAL ASSURANCE CRITERION–TWENTY YEARS OF USE AND ABUSE , 2003 .
[24] Jen-Kuang Huang,et al. Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method , 1995 .
[25] Quan Wang,et al. Dynamic stability analysis of a pressurized FG-CNTRC cylindrical shell interacting with supersonic airflow , 2017 .
[26] P. Šidlof,et al. Experimental investigation of flow-induced vibration of a pitch–plunge NACA 0015 airfoil under deep dynamic stall , 2016 .
[27] P. Chen. Damping Perturbation Method for Flutter Solution: The g-Method , 2000 .