Teng Zhang

ORCID: 0000-0001-8867-7750
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About
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Research Areas
  • Corrosion Behavior and Inhibition
  • Fatigue and fracture mechanics
  • Concrete Corrosion and Durability
  • High-Velocity Impact and Material Behavior
  • Non-Destructive Testing Techniques
  • Hydrogen embrittlement and corrosion behaviors in metals
  • Aluminum Alloy Microstructure Properties
  • Aluminum Alloys Composites Properties
  • Metal and Thin Film Mechanics
  • Mechanical Behavior of Composites
  • Structural Load-Bearing Analysis
  • Composite Structure Analysis and Optimization
  • Photoacoustic and Ultrasonic Imaging
  • Advanced Sensor and Energy Harvesting Materials
  • Smart Materials for Construction
  • Probabilistic and Robust Engineering Design
  • Ultrasound Imaging and Elastography
  • Nuclear materials and radiation effects
  • Adhesion, Friction, and Surface Interactions
  • Ultrasonics and Acoustic Wave Propagation
  • Structural Response to Dynamic Loads
  • Metallurgy and Material Forming
  • Metal Forming Simulation Techniques
  • Machine Fault Diagnosis Techniques
  • Microstructure and mechanical properties

Southwestern Institute of Physics
2023-2024

Air Force Engineering University
2013-2024

University of Cambridge
2023-2024

Chinese People's Liberation Army
2023

China Electric Power Research Institute
2022

Massachusetts Institute of Technology
2015

Fuzhou University
2009-2012

Multiple cold expansion holes are widely used in connection areas of aircraft structures, order to achieve uniform load transfer the skin or parts. Split sleeve (SSCE) is enhance fatigue life fastener by applying compressive residual stresses around holes. In this study, finite element method (FEM) was research distribution and variation along hole edges 7075AA single-hole multi-hole (CE) specimens. Full-field strain measurements specimens were performed using two-dimensional digital image...

10.3390/ma16031109 article EN Materials 2023-01-27

The atmospheric corrosion of epoxy prime coated aluminum alloy 7075-T6 exposed for 7, 12 and 20 years was investigated. remaining thicknesses coatings macroscopically intact coating areas followed a normal distribution decreased linearly. EIS results demonstrated that the resistance with exposure time. After exposure, had lost its protection as cracks existed within exfoliation occurred on substrate. substrate sensitive to through metallographic TEM analysis. products were mainly hydroxides...

10.3390/ma11060965 article EN Materials 2018-06-07

In this paper, by establishing a fragmented field of prefabricated fragment warhead and simulating the intersection aircraft under dynamic conditions, determination distribution vulnerable parts specific is realized. On basis, structural characteristic test pieces were tested with high-velocity impact experiments based on two-stage light-gas gun. Based FEM-SPH self-adaptive method, numerical simulation model high reduction degree was established. Combined experimental results, damage mode...

10.1016/j.aej.2022.07.040 article EN cc-by-nc-nd Alexandria Engineering Journal 2022-08-03

10.1007/s11665-015-1541-y article EN Journal of Materials Engineering and Performance 2015-05-05

Aircraft are subjected to extreme weather conditions in coastal areas. This study reports long-term atmospheric exposure tests carried out on an epoxy primer-coated aluminum alloy a environment for 7, 12, and 20 years. The micromorphology characteristics of the section surface, products corrosion, electrochemical impedance, molecular structure coated specimens were examined through spectrophotometer, scanning electron microscopy (SEM), atomic force (AFM), X-ray diffraction (XRD), impedance...

10.3390/coatings11020237 article EN Coatings 2021-02-17

To investigate the effect of alternate corrosion and fatigue on crack growth characterization 2024-T4 aluminum alloy, pure test, “corrosion + fatigue” test (commonly known as pre-corrosion fatigue), “fatigue alternating single-sided notched specimen alloy were carried out. The life is longer than that when time same. And more times alternating, will be. This mainly because rate change suddenly, which have a certain hysteresis growth. fracture morphology characteristics examined by scanning...

10.1155/2020/7314241 article EN Mathematical Problems in Engineering 2020-03-12

Advanced crack monitoring technique is the cornerstone of aircraft structural health monitoring. To achieve real-time metal structures in course service, a new method proposed based on Cu coating sensor and electrical potential difference principle. Firstly, insulation treatment process was used to prepare dielectric layer substrate, such as an anodizing 2A12-T4 aluminum alloy then deposited structure fatigue critical parts by pulsed bias arc ion plating technology. Secondly, damage...

10.1016/j.cja.2015.02.016 article EN cc-by-nc-nd Chinese Journal of Aeronautics 2015-04-11

The recent patents on corrosion resistant coatings were reviewed in this paper.The materials of components, e.g., metals and alloys, ceramics, polymers as well composite materials, developed for environmental, economic other concerns discussed.In addition, the novel methods forming coatings, including powder floating by vibration precursor gas, some widely employed industrial applications also included to provide useful information colleagues.

10.2174/1877610800901010001 article EN Recent Patents on Corrosion Science 2009-10-29

A two-stage light gas gun was used to conduct a high-velocity impact test on the aircraft’s typical composite/metal connecting structure (CFRP/AL). The battle damage simulations for CFRP/AL were carried out under different intersection conditions. Then, morphology and mechanism of prefabricated spherical fragments structures, dynamic process hyper-velocity impact, formation debris clouds secondary component structures investigated. Next, based X-ray computerized tomography (CT), mode areas...

10.3390/app12189268 article EN cc-by Applied Sciences 2022-09-15

Particulate fouling is a common in heat exchange equipment, it causes tube corrosion and increases flow resistance. the hidden danger of equipment requires high treatment costs. In this paper, novel Ni−P−TiO2 composite coating prepared on 316 stainless steel using electroless plating inhibition characteristics are studied dynamic monitoring experimental system. The results show that thermal resistance obviously lower than under same working conditions. With increase cooling water velocity...

10.3390/coatings13020274 article EN Coatings 2023-01-25

Abstract The investigation of fatigue crack propagation and fracture mechanisms in high-thickness metal plates holds pivotal importance the advancement a three-dimensional damage tolerance assessment methodology. This research also bears significant implications for ensuring safe operation large-scale mechanical equipment. In this study, we examine influence specimen thickness on evolution shapes an aluminum alloy. Fatigue growth tests were conducted single-edge notch tension specimens to...

10.1088/1742-6596/2671/1/012024 article EN Journal of Physics Conference Series 2024-01-01
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