Zhengqiang Cheng
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View article: Fatigue Reliability Evaluation of Composite Structures with Low-Velocity Impact Damage
Fatigue Reliability Evaluation of Composite Structures with Low-Velocity Impact Damage Open
View article: Advanced computational modelling of composite materials
Advanced computational modelling of composite materials Open
This review paper presents an overview of computational methods for modelling the failure of composite materials, with a focus on fracture modelling. The paper begins by discussing the principles and concepts of continuum damage mechanics …
View article: Dynamic Constitutive Model and Finite Element Simulation of Impact Loading of 6008 Aluminum Alloy Based on Precipitation Hardening and Damage
Dynamic Constitutive Model and Finite Element Simulation of Impact Loading of 6008 Aluminum Alloy Based on Precipitation Hardening and Damage Open
View article: Modelling fatigue behaviours and lifetimes of novel GLARE laminates under random loading spectrum
Modelling fatigue behaviours and lifetimes of novel GLARE laminates under random loading spectrum Open
View article: Modelling pre-fatigue, low-velocity impact and post-impact fatigue behaviours of composite helicopter tail structures under multipoint coordinated loading spectrum
Modelling pre-fatigue, low-velocity impact and post-impact fatigue behaviours of composite helicopter tail structures under multipoint coordinated loading spectrum Open
View article: Modelling Pre-fatigue, Low-velocity Impact and Fatigue behaviours of Composite Helicopter Tail Structures under Multipoint Coordinated Loading Spectrum
Modelling Pre-fatigue, Low-velocity Impact and Fatigue behaviours of Composite Helicopter Tail Structures under Multipoint Coordinated Loading Spectrum Open
This paper aims to numerically study the pre-fatigue, low-velocity impact (LVI) and fatigue progressive damage behaviours of a full-scale composite helicopter tail structure under multipoint coordinated loading spectrum. First, a fatigue p…
View article: Progressive Damage Modelling and Fatigue Life Prediction of Plain-weave Composite Laminates with Low-velocity Impact Damage
Progressive Damage Modelling and Fatigue Life Prediction of Plain-weave Composite Laminates with Low-velocity Impact Damage Open
This paper developed a fatigue-driven residual strength model considering the effects of low-velocity impact (LVI) damage and stress ratio. New fatigue failure criteria based on fatigue-driven residual strength concept and fatigue progress…
View article: Progressive damage behaviors of woven composite laminates subjected to LVI, TAI and CAI
Progressive damage behaviors of woven composite laminates subjected to LVI, TAI and CAI Open
This paper seeks to deal with progressive damage behaviors of woven composite laminates subjected to low-velocity impact (LVI), tension-after-impact (TAI) and compression-after-impact (CAI). The LVI, TAI and CAI tests were conducted on wov…