Z
Zengshun Chen
Researcher at Chongqing University
Publications - 86
Citations - 1032
Zengshun Chen is an academic researcher from Chongqing University. The author has contributed to research in topics: Wind tunnel & Aerodynamic force. The author has an hindex of 13, co-authored 61 publications receiving 519 citations. Previous affiliations of Zengshun Chen include Hong Kong University of Science and Technology & Chongqing Jiaotong University.
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Deployment of a Smart Structural Health Monitoring System for Long-Span Arch Bridges: A Review and a Case Study.
TL;DR: The paper reviews the recent progress of the SHM technology that has been applied to long-span bridges and introduces the deployment and investigation of a SHM system for long- span arch bridges.
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Mechanical behavior of multilayer GO carbon-fiber cement composites
TL;DR: In this article, the compressive strength and the flexural tensile strength of multilayer carbon-fiber cement composites were experimentally investigated, and the results were explained with respect to the mechanical behavior of GO cement specimens with incorporating different percentages of GO and the microstructures observed by Scanning Electron Microscopy (SEM).
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Application of the Local Fractional Series Expansion Method and the Variational Iteration Method to the Helmholtz Equation Involving Local Fractional Derivative Operators
TL;DR: In this paper, the authors investigate solutions of the Helmholtz equation involving local fractional derivative operators and make use of the series expansion method and the variational iteration method, which are based upon the local fractionals derivative operators.
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A perspective on the aerodynamics and aeroelasticity of tapering: Partial reattachment
TL;DR: In this paper, the effects of tapering on aerodynamic, aero-elasticity, and fluid-structure interaction of buildings have been investigated through wind tunnel tests, specifically considering different wind attack angles, wind velocities, and structural rigidities.
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Measurement of unsteady aerodynamic force on a galloping prism in a turbulent flow: A hybrid aeroelastic-pressure balance
TL;DR: In this paper, a hybrid aeroelastic-pressure balance (HAPB) technique was proposed for the measurement of unsteady aerodynamic force on a galloping prism, which can accurately predict the galloping response of the test model whereas the classical quasi-steady theory fails for the prediction.