Xiaowei Chen

ORCID: 0000-0001-9756-5232
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About
Contact & Profiles
Research Areas
  • High-Velocity Impact and Material Behavior
  • Structural Response to Dynamic Loads
  • Fluid Dynamics Simulations and Interactions
  • Energetic Materials and Combustion
  • Electromagnetic Launch and Propulsion Technology
  • Laser-Plasma Interactions and Diagnostics
  • Rock Mechanics and Modeling
  • High-pressure geophysics and materials
  • Planetary Science and Exploration
  • Cellular and Composite Structures
  • Metallic Glasses and Amorphous Alloys
  • Fluid Dynamics and Heat Transfer
  • Nuclear Materials and Properties
  • Geophysical Methods and Applications
  • Combustion and Detonation Processes
  • Numerical methods in engineering
  • Astro and Planetary Science
  • High-Temperature Coating Behaviors
  • Hydraulic Fracturing and Reservoir Analysis
  • Polymer Foaming and Composites
  • Nanocomposite Films for Food Packaging
  • Military Defense Systems Analysis
  • Fire dynamics and safety research
  • Metal Alloys Wear and Properties
  • Electromagnetic wave absorption materials

Beijing Institute of Technology
2007-2024

Zhengzhou University
2024

University of Science and Technology Beijing
2015-2021

Huanghe Science and Technology College
2019

University of Oklahoma
2019

Sichuan Research Center of New Materials
2017-2019

Peking University
2017-2018

China Academy of Engineering Physics
2006-2017

University of Science and Technology of China
2017

Chinese Academy of Engineering
2008

10.1016/j.ijhydene.2020.10.097 article EN International Journal of Hydrogen Energy 2020-11-20

Whipple shield, a dual-wall system, as well its improved structures, is widely applied to defend the hypervelocity impact of space debris (projectile). This paper reviews studies about mechanism and process protection against impacts using shield. Ground-based experiment numerical simulation for are introduced briefly. Three steps shield discussed in order, including interaction between projectile bumper, movement diffusion cloud, cloud rear plate. Potential improvements performance focusing...

10.1016/j.dt.2020.11.005 article EN cc-by-nc-nd Defence Technology 2020-11-24

10.1016/j.ijimpeng.2008.01.002 article EN International Journal of Impact Engineering 2008-02-08

This study investigates how the debris cloud structure and hazardous fragment distribution vary with attack angle by simulating a circular cylinder projectile hypervelocity impinging on thin plate using finite element–smoothed particle hydrodynamics (FE-SPH) adaptive method. Based comparison analysis of experimental simulation results, FE-SPH method was applied to address yaw impact problem, variation law obtained. The screening criterion at is given analyzing formation obtained method,...

10.1016/j.dt.2022.09.010 article EN cc-by-nc-nd Defence Technology 2022-09-26

10.1016/j.ijimpeng.2023.104803 article EN International Journal of Impact Engineering 2023-10-09

The debris cloud generated by the hypervelocity impact (HVI) of orbiting space directly threatens spacecraft. A full understanding damage mechanism rear plate is useful for optimal design protective structures. In this study, yaw a cylindrical aluminum projectile on double-layer simulated FE-SPH adaptive method, and process under analyzed based structure. can be divided into main stage structural response plate. lasts short time basis damage. structure response, continuous deformation...

10.1016/j.dt.2024.01.005 article EN cc-by-nc-nd Defence Technology 2024-01-30

Shaped charge liner (SCL) has been extensively applied in oil recovery and defense industries. Achieving superior penetration capability through optimizing SCL structures presents a substantial challenge due to intricate rate-dependent processes involving detonation-driven collapse, high-speed jet stretching, penetration. This study introduces an innovative optimization strategy for that employs efficiency as the primary objective function. The combines experimentally validated finite...

10.1016/j.dt.2024.04.006 article EN cc-by-nc-nd Defence Technology 2024-04-26

10.1016/j.ijimpeng.2020.103727 article EN International Journal of Impact Engineering 2020-09-19
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