Nonlinear bending analysis of FG-CNT reinforced composite thick plates resting on Pasternak foundations using the element-free IMLS-Ritz method LW Zhang, ZG Song, KM Liew Composite Structures 128, 165-175, 2015 | 164 | 2015 |
Active aeroelastic flutter analysis and vibration control of supersonic composite laminated plate ZG Song, FM Li Composite Structures 94 (2), 702-713, 2012 | 151 | 2012 |
Vibration analysis of CNT-reinforced functionally graded composite cylindrical shells in thermal environments ZG Song, LW Zhang, KM Liew International Journal of Mechanical Sciences 115, 339-347, 2016 | 132 | 2016 |
Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow LW Zhang, ZG Song, KM Liew Computer Methods in Applied Mechanics and Engineering 300, 427-441, 2016 | 123 | 2016 |
State-space Levy method for vibration analysis of FG-CNT composite plates subjected to in-plane loads based on higher-order shear deformation theory LW Zhang, ZG Song, KM Liew Composite Structures 134, 989-1003, 2015 | 122 | 2015 |
Optimal shape control of CNT reinforced functionally graded composite plates using piezoelectric patches LW Zhang, ZG Song, KM Liew Composites Part B: Engineering 85, 140-149, 2016 | 111 | 2016 |
Modeling of dynamic responses of CNT-reinforced composite cylindrical shells under impact loads LW Zhang, ZG Song, P Qiao, KM Liew Computer Methods in Applied Mechanics and Engineering 313, 889-903, 2017 | 110 | 2017 |
Active aeroelastic flutter analysis and vibration control of supersonic beams using the piezoelectric actuator/sensor pairs ZG Song, FM Li Smart Materials and Structures 20 (5), 055013, 2011 | 86 | 2011 |
Flutter and thermal buckling control for composite laminated panels in supersonic flow FM Li, ZG Song Journal of Sound and Vibration 332 (22), 5678-5695, 2013 | 82 | 2013 |
Active vibration control of CNT-reinforced composite cylindrical shells via piezoelectric patches ZG Song, LW Zhang, KM Liew Composite Structures 158, 92-100, 2016 | 76 | 2016 |
Active vibration control of CNT reinforced functionally graded plates based on a higher-order shear deformation theory ZG Song, LW Zhang, KM Liew International Journal of Mechanical Sciences 105, 90-101, 2016 | 75 | 2016 |
Active vibration control of conical shells using piezoelectric materials FM Li, ZG Song, ZB Chen Journal of Vibration and Control 18 (14), 2234-2256, 2012 | 71 | 2012 |
Dynamic responses of CNT reinforced composite plates subjected to impact loading ZG Song, LW Zhang, KM Liew Composites Part B: Engineering 99, 154-161, 2016 | 65 | 2016 |
Investigations on the influences of elastic foundations on the aerothermoelastic flutter and thermal buckling properties of lattice sandwich panels in supersonic airflow YY Chai, ZG Song, FM Li Acta Astronautica 140, 176-189, 2017 | 57 | 2017 |
A new method of smart and optimal flutter control for composite laminated panels in supersonic airflow under thermal effects ZG Song, FM Li, E Carrera, P Hagedorn Journal of Sound and Vibration 414, 218-232, 2018 | 54 | 2018 |
Aeroelastic analysis of CNT reinforced functionally graded composite panels in supersonic airflow using a higher-order shear deformation theory ZG Song, LW Zhang, KM Liew Composite Structures 141, 79-90, 2016 | 50 | 2016 |
Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow FM Li, ZG Song Acta Mechanica 225, 3339-3351, 2014 | 49 | 2014 |
Investigations on the flutter properties of supersonic panels with different boundary conditions ZG Song, FM Li International Journal of Dynamics and Control 2, 346-353, 2014 | 49 | 2014 |
Aerothermoelastic analysis of nonlinear composite laminated panel with aerodynamic heating in hypersonic flow ZG Song, FM Li Composites Part B: Engineering 56, 830-839, 2014 | 49 | 2014 |
Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams ZG Song, FM Li Nonlinear Dynamics 76, 57-68, 2014 | 48 | 2014 |