Wei Xia
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Research Subjects
Wei Xia has a total of 83 co-authors. Here are the top co-authors by number of shared publications:
Shuling Hu
Xi’an Jiaotong University
8 shared publications- Kun Wang
State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong University, Xi’an 710049, People’s Republic of China
5 shared publications Datao Li
4 shared publicationsShengping Shen
State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace, Xi’an Jiaotong University, No. 28, Xianning West Road, Xi’an, Shaanxi 710049, P. R. China
4 shared publicationsZuojia Liao
Xi’an Jiaotong University
4 shared publications- Shuling Hu
State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong University, Xi’an 710049, People’s Republic of China
3 shared publications
Latest Publications
- 2 January 2026
- Published by Springer Nature
- p. 310-321
Mechanical Performance Analysis of Reinforced Quad-Star Honeycomb with Zero Poisson’s Ratio
- 2 January 2026
- Published by Springer Nature
- p. 310-321
Mechanical Performance Analysis of Reinforced Quad-Star Honeycomb with Zero Poisson’s Ratio
- 16 November 2025
- Published by Springer Nature
- p. 623-637
Application of Flexural Hinges in Variable Camber Wing: Morphing Capability and Aerodynamic Performance Evaluation
- 16 November 2025
- Published by Springer Nature
- p. 623-637
Application of Flexural Hinges in Variable Camber Wing: Morphing Capability and Aerodynamic Performance Evaluation
- 16 November 2025
- Published by Springer Nature
- p. 664-673
Design of Ground Test Model for Wing-Aileron Flutter with Freeplay Effects
- 16 November 2025
- Published by Springer Nature
- p. 664-673
Design of Ground Test Model for Wing-Aileron Flutter with Freeplay Effects
- 16 November 2025
- Published by Springer Nature
- p. 638-651
Numerical Simulation Analysis and Experimental Design for Aerodynamic Performance of Hovering Flapping Wings
- 16 November 2025
- Published by Springer Nature
- p. 638-651
Numerical Simulation Analysis and Experimental Design for Aerodynamic Performance of Hovering Flapping Wings
- 29 October 2025
- Published by Wiley in Energy Technology
- Vol. 14 (1)
Flow‐Induced Vibration of V‐Shape Prism and its Application in Wind Energy Conversion
Inspired by the palm leaf structure, this work developed a novel V‐shape prism. The flow‐induced vibration (FIV) mechanism of the V‐shape prism under typical windward angles (α = 0°, 90°, and 180°) is studied by numerical simulation. The impact of wind speed and direction on vibration amplitude, frequency, force coefficient, phase, and vorticity contours is analyzed. The V‐shape prism undergoes vortex‐induced vibration (VIV) or galloping with the change of wind speed and direction. The vibration amplitude in galloping mode is higher than that in VIV mode. The wind speed and direction have little effect on the vibration frequency in galloping mode, while the vibration frequency in VIV mode is determined by the vortex shedding. The transform of the prism vibration mode is accompanied by a change of phase lag and vortex structure. The V‐shape prism at α = 0° exhibits a significantly greater vibration amplitude and energy conversion efficiency compared to both the square prism and other windward angles. The highest energy conversion efficiency of the V‐shape prism is 69.2%, which is 22.2 times that of the square prism device. This work presents the potential application of a V‐shape prism in the future design of FIV energy harvesters.
- 29 October 2025
- Published by Wiley in Energy Technology
- Vol. 14 (1)
Flow‐Induced Vibration of V‐Shape Prism and its Application in Wind Energy Conversion
Inspired by the palm leaf structure, this work developed a novel V‐shape prism. The flow‐induced vibration (FIV) mechanism of the V‐shape prism under typical windward angles (α = 0°, 90°, and 180°) is studied by numerical simulation. The impact of wind speed and direction on vibration amplitude, frequency, force coefficient, phase, and vorticity contours is analyzed. The V‐shape prism undergoes vortex‐induced vibration (VIV) or galloping with the change of wind speed and direction. The vibration amplitude in galloping mode is higher than that in VIV mode. The wind speed and direction have little effect on the vibration frequency in galloping mode, while the vibration frequency in VIV mode is determined by the vortex shedding. The transform of the prism vibration mode is accompanied by a change of phase lag and vortex structure. The V‐shape prism at α = 0° exhibits a significantly greater vibration amplitude and energy conversion efficiency compared to both the square prism and other windward angles. The highest energy conversion efficiency of the V‐shape prism is 69.2%, which is 22.2 times that of the square prism device. This work presents the potential application of a V‐shape prism in the future design of FIV energy harvesters.
- 16 October 2025
- Published by IOP Publishing in Journal of Physics D: Applied Physics
- Vol. 58 (42) , 425502
Enhancing energy harvesting efficiency by utilizing twisting kinematics in flutter-driven wind energy harvester
Vibration-driven wind energy harvesters (WEHs) are much eco-friendly than wind turbines because of their quiet and safe operation for surrounding humans and animals. However, the low energy harvesting efficiency limits the wide application of vibration-driven WEHs. The present study designs a flutter-driven WEH based on the decoupling structure between bending and twisting stiffnesses, which produces predictable violent oscillation in the wind. The WEH electromechanical coupling model considering the aeroelastic effects is established based on the Hamiltonian principle. The effects of bending and twisting stiffnesses on the flutter on-set speed, flutter frequency, and electric output are analyzed numerically. The wind energy harvesting performance is evaluated in a low-speed wind tunnel. The electric outputs bending and twisting kinematics are compared by sticking two lead zirconate titanate patches on corresponding positions of the decoupling structure. The test results show that the electric output power densities of present WEH in 9 m s−1 wind from bending and twisting kinematics are 1497.33 μW cm−3 and 200.22 μW cm−3, respectively. The bending and twisting energy conversion efficiencies are 0.31% and 29.6%, respectively. The effective enhancement of wind energy harvesting efficiency is achieved by adding twisting kinematics into the WEH. Up to 13.4% additional output power is obtained in the present WEH compared against the WEH with only bending kinematics. With the additional twisting kinematic energy, the present flutter-driven energy harvester is capable of lighting one 10 μW light-emitting diode at a wind speed of 6 m s−1. This demonstration gives a potential way of enhancing the WEH’s energy harvesting efficiency. Future work would focus on the structural design and optimization with detailed applications.
- 16 October 2025
- Published by IOP Publishing in Journal of Physics D: Applied Physics
- Vol. 58 (42) , 425502
Enhancing energy harvesting efficiency by utilizing twisting kinematics in flutter-driven wind energy harvester
Vibration-driven wind energy harvesters (WEHs) are much eco-friendly than wind turbines because of their quiet and safe operation for surrounding humans and animals. However, the low energy harvesting efficiency limits the wide application of vibration-driven WEHs. The present study designs a flutter-driven WEH based on the decoupling structure between bending and twisting stiffnesses, which produces predictable violent oscillation in the wind. The WEH electromechanical coupling model considering the aeroelastic effects is established based on the Hamiltonian principle. The effects of bending and twisting stiffnesses on the flutter on-set speed, flutter frequency, and electric output are analyzed numerically. The wind energy harvesting performance is evaluated in a low-speed wind tunnel. The electric outputs bending and twisting kinematics are compared by sticking two lead zirconate titanate patches on corresponding positions of the decoupling structure. The test results show that the electric output power densities of present WEH in 9 m s−1 wind from bending and twisting kinematics are 1497.33 μW cm−3 and 200.22 μW cm−3, respectively. The bending and twisting energy conversion efficiencies are 0.31% and 29.6%, respectively. The effective enhancement of wind energy harvesting efficiency is achieved by adding twisting kinematics into the WEH. Up to 13.4% additional output power is obtained in the present WEH compared against the WEH with only bending kinematics. With the additional twisting kinematic energy, the present flutter-driven energy harvester is capable of lighting one 10 μW light-emitting diode at a wind speed of 6 m s−1. This demonstration gives a potential way of enhancing the WEH’s energy harvesting efficiency. Future work would focus on the structural design and optimization with detailed applications.
- 5 August 2025
- Published by Elsevier in Aerospace Science and Technology
- Vol. 167
Flapping propulsion of low aspect-ratio wing with morphing trailing edge: Lattice Boltzmann simulation
- 5 August 2025
- Published by Elsevier in Aerospace Science and Technology
- Vol. 167
Flapping propulsion of low aspect-ratio wing with morphing trailing edge: Lattice Boltzmann simulation
- 11 January 2024
- Published by Elsevier in Construction and Building Materials
- Vol. 413, 134925
Investigations on tensile mechanical properties of rigid insulation tile materials at elevated temperatures based on digital image correlation algorithm
- 11 January 2024
- Published by Elsevier in Construction and Building Materials
- Vol. 413, 134925
Investigations on tensile mechanical properties of rigid insulation tile materials at elevated temperatures based on digital image correlation algorithm
- 19 December 2023
- Published by Springer Nature
- p. 416-424
Body Freedom Flutter of Carried Flyer on a Twin-Fuselage Aircraft
- 19 December 2023
- Published by Springer Nature
- p. 416-424
Body Freedom Flutter of Carried Flyer on a Twin-Fuselage Aircraft
- Open Access
- 16 October 2023
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 37 (2) , 100-122
Aerodynamic optimization of an adaptive flap for next-generation green aircraft
- 16 October 2023
- Published by Elsevier in Chinese Journal of Aeronautics
- Vol. 37 (2) , 100-122
Open AccessAerodynamic optimization of an adaptive flap for next-generation green aircraft