Analytical model of bolted disk–drum joints and its application to dynamic analysis of jointed rotor ZY Qin, QK Han, FL Chu Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2014 | 155 | 2014 |
Vibration studies of rotating cylindrical shells with arbitrary edges using characteristic orthogonal polynomials in the Rayleigh–Ritz method S Sun, D Cao, Q Han International Journal of Mechanical Sciences 68, 180-189, 2013 | 137 | 2013 |
Fixed-point rubbing fault characteristic analysis of a rotor system based on contact theory H Ma, C Shi, Q Han, B Wen Mechanical Systems and Signal Processing 38 (1), 137-153, 2013 | 125 | 2013 |
Dynamic characteristics analysis of a rotor–stator system under different rubbing forms H Ma, Q Zhao, X Zhao, Q Han, B Wen Applied Mathematical Modelling 39 (8), 2392-2408, 2015 | 99 | 2015 |
Nonlinear vibrations of fiber-reinforced composite cylindrical shells with bolt loosening boundary conditions H Li, H Lv, H Sun, Z Qin, J Xiong, Q Han, J Liu, X Wang Journal of Sound and Vibration 496, 115935, 2021 | 96 | 2021 |
Nonlinear vibration characteristics of fibre reinforced composite cylindrical shells in thermal environment H Li, H Lv, J Gu, J Xiong, Q Han, J Liu, Z Qin Mechanical Systems and Signal Processing 156, 107665, 2021 | 85 | 2021 |
Remaining life prediction method for rolling bearing based on the long short-term memory network F Wang, X Liu, G Deng, X Yu, H Li, Q Han Neural processing letters 50, 2437-2454, 2019 | 85 | 2019 |
Time–frequency features of two types of coupled rub-impact faults in rotor systems H Ma, T Yu, Q Han, Y Zhang, B Wen, C Xuelian Journal of sound and vibration 321 (3-5), 1109-1128, 2009 | 83 | 2009 |
A revised model for rubbing between rotating blade and elastic casing H Ma, X Tai, Q Han, Z Wu, D Wang, B Wen Journal of Sound and Vibration 337, 301-320, 2015 | 82 | 2015 |
A model reduction approach for the vibration analysis of hydraulic pipeline system in aircraft P Gao, J Zhai, Y Yan, Q Han, F Qu, X Chen Aerospace Science and Technology 49, 144-153, 2016 | 80 | 2016 |
Vibration and damping analysis of the bladed disk with damping hard coating on blades Y Chen, J Zhai, Q Han Aerospace Science and Technology 58, 248-257, 2016 | 76 | 2016 |
Nonlinear vibration analysis of fiber reinforced composite cylindrical shells with partial constrained layer damping treatment H Li, Z Wang, H Lv, Z Zhou, Q Han, J Liu, Z Qin Thin-Walled Structures 157, 107000, 2020 | 65 | 2020 |
Periodic motions of a dual-disc rotor system with rub-impact at fixed limiter Q Han, Z Zhang, B Wen Proceedings of the Institution of Mechanical Engineers, Part C: Journal of …, 2008 | 62 | 2008 |
Vibration and damping analysis of cylindrical shell treated with viscoelastic damping materials under elastic boundary conditions via a unified Rayleigh-Ritz method X Song, T Cao, P Gao, Q Han International Journal of Mechanical Sciences 165, 105158, 2020 | 57 | 2020 |
Investigation on thermal behavior and temperature distribution of bearing inner and outer rings X Zhou, H Zhang, X Hao, X Liao, Q Han Tribology International 130, 289-298, 2019 | 55 | 2019 |
Traveling wave analysis of rotating cross-ply laminated cylindrical shells with arbitrary boundaries conditions via Rayleigh–Ritz method X Song, J Zhai, Y Chen, Q Han Composite Structures 133, 1101-1115, 2015 | 53 | 2015 |
Vibration reduction of the blisk by damping hard coating and its intentional mistuning design Y Chen, H Wu, J Zhai, H Chen, Q Zhu, Q Han Aerospace Science and Technology 84, 1049-1058, 2019 | 52 | 2019 |
An analytical solution for a multilayered magneto-electro-elastic circular plate under simply supported lateral boundary conditions R Wang, Q Han, E Pan Smart Materials and Structures 19 (6), 065025, 2010 | 52 | 2010 |
Estimate of material property of carbon nanotubes via nonlocal elasticity Q Wang, QK Han, BC Wen Adv. Theor. Appl. Mech 1 (1), 1-10, 2008 | 52 | 2008 |
A dynamic modeling approach for nonlinear vibration analysis of the L-type pipeline system with clamps C Qingdong, Z Jin, MA Hui, LI Kun, HAN Qingkai Chinese Journal of Aeronautics 33 (12), 3253-3265, 2020 | 51 | 2020 |