Browsing by Author Tong, Liyong

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Issue DateTitleAuthor(s)Citation
20152D fracture analysis of magnetoelectroelastic composites by the SBFEMLi, Chao; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic Eng2D fracture analysis of magnetoelectroelastic composites by the SBFEM, Composite Structures, vol.132, 2015, 2015,pp 984-994
20113D Model of Coupled Multi-physics Fields for PLZT Ceramics and Its Applications to Photostrictive PlatesLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic Eng3D Model of Coupled Multi-physics Fields for PLZT Ceramics and Its Applications to Photostrictive Plates, Journal of Intelligent Material Systems and Structures, vol.22, 1, 2011,pp 17-30
2004An Accurate Laminated Element For Piezoelectric Smart Beams Including Peel StressLuo, Quan; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAn Accurate Laminated Element For Piezoelectric Smart Beams Including Peel Stress, Computational Mechanics, vol.33,(2),2004,pp 108-120
2007Active vibration control of a laminated composite beam using MFRC patchesTan, Ping; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngActive vibration control of a laminated composite beam using MFRC patches, CD-ROM Proceedings of The Sixteenth International Conference on Composite Materials, July 8-13, 2007: Kyoto, Japan, vol.cdrom,(),2007,pp 1-10
2013Adaptive pressure-controlled cellular structures for shape morphing I: design and analysisLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAdaptive pressure-controlled cellular structures for shape morphing I: design and analysis, Smart Materials and Structures, vol.22, 5, 2013,pp 1-16
2013Adaptive pressure-controlled cellular structures for shape morphing: II. Numerical and experimental validationLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAdaptive pressure-controlled cellular structures for shape morphing: II. Numerical and experimental validation, Smart Materials and Structures, vol.22, N/A, 2013,pp 1-12
2004Adhesive Element Modelling And Weighted Static Shape Control Of Composite Plates With Piezoelectric Actuator PatchesSun, Dongchang; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAdhesive Element Modelling And Weighted Static Shape Control Of Composite Plates With Piezoelectric Actuator Patches, International Journal for Numerical Methods in Engineering, vol.60,(11),2004,pp 1911-1932
2003Adhesive elements for stress analysis of bonded patch to curved thin-walled structuresSun, Xiannian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAdhesive elements for stress analysis of bonded patch to curved thin-walled structures, Computational Mechanics, vol.30,(2),2003,pp 143-154
2004An Adhesively Laminated Plate Element For Pzt Smart PlatesLuo, Quan; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAn Adhesively Laminated Plate Element For Pzt Smart Plates, Computational Mechanics, vol.34,(3),2004,pp 224-236
2016An algorithm for eradicating the effects of void elements on structural topology optimization for nonlinear complianceLuo, Quantian; Tong, Liyong; Aerospace Mech & Mtronic Eng; Aerospace Mech & Mtronic EngAn algorithm for eradicating the effects of void elements on structural topology optimization for nonlinear compliance, Structural and Multidisciplinary Optimization, vol.53, 4, 2016,pp 695-714
2008Analysis of cracked lap shear (CLS) jointsLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalysis of cracked lap shear (CLS) joints in Modeling of Adhesively Bonded Joints, Springer, 2008, pp. 22-51
2005Analysis of energy release rate for fatigue cracked metal-to-metal double-lap shear jointsCheuk, Po; Tong, Liyong; Rider, A. N.; Wang, Jie Jin; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalysis of energy release rate for fatigue cracked metal-to-metal double-lap shear joints, International Journal of Adhesion and Adhesives, vol.25,(2),2005,pp 181-191
2012Analytic formulas of energy release rates for delamination using a global–local methodLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalytic formulas of energy release rates for delamination using a global–local method, International Journal of Solids and Structures, vol.49, 23–24, 2012,pp 3335-3344
2011Analytical Approach to Joint DesignLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalytical Approach to Joint Design in Handbook of Adhesion Technology, Springer, 2011, pp. 597-627
2008Analytical solutions for adhesive composite joints considering large deflection and transverse shear deformation in adherendsLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalytical solutions for adhesive composite joints considering large deflection and transverse shear deformation in adherends, International Journal of Solids and Structures, vol.45, 22-23, 2008,pp 5914-5935
2009Analytical solutions for nonlinear analysis of composite single-lap adhesive jointsLuo, Quantian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngAnalytical solutions for nonlinear analysis of composite single-lap adhesive joints, International Journal of Adhesion and Adhesives, vol.29, N/A,pp N/A-154
2017Application of FEM/IBEM combined with PEM for acoustic radiation and sensitivity analysis of a randomly excited structureTong, Liyong; Liu, Baoshan; Zhao, Guozhong; Aerospace, Mechanical and Mechatronic EngineeringApplication of FEM/IBEM combined with PEM for acoustic radiation and sensitivity analysis of a randomly excited structure, Noise Control Engineering Journal, vol.65, 4, 2017,pp 266-274
2004Bending Effect Of Through-Thickness Reinforcement Rods On Mode I Delamination Toughness Of Dcb Specimen. I. Linearly Elastic And Rigid-Perfectly Plastic ModelsSun, Xiannian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngBending Effect Of Through-Thickness Reinforcement Rods On Mode I Delamination Toughness Of Dcb Specimen. I. Linearly Elastic And Rigid-Perfectly Plastic Models, International Journal of Solids and Structures, vol.41,(24-25),2004,pp 6831-6852
2007Bending effect of through-thickness reinforcement rods on mode II delamination toughness of ENF specimen: Elastic and rigid-perfectly plastic analysesSun, Xiannian; Tong, Liyong; Aerospace Mech & M'tronic Eng; Aerospace Mech & M'tronic EngBending effect of through-thickness reinforcement rods on mode II delamination toughness of ENF specimen: Elastic and rigid-perfectly plastic analyses, Composites Part A-Applied Science and Manufacturing, vol.38,(2),2007,pp 323-336
2016A bridging law and its application to the analysis of toughness of carbon nanotube-reinforced composites and pull-out of fibres grafted with nanotubesTong, Liyong; Wang, Jianxiang; Karihaloo, Bhushan; Aerospace Mech & Mtronic Eng; Aerospace Mech & Mtronic EngA bridging law and its application to the analysis of toughness of carbon nanotube-reinforced composites and pull-out of fibres grafted with nanotubes, Archive of Applied Mechanics, vol.86, 1-2, 2016,pp 361-373