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- W2373754471 abstract "Based on the 3D visco-elastic constitutive equations of composite,a finite element model was proposed for the damage analysis of fiber reinforce composite laminates under high velocity impact.The cohesive elements were involved between layers to simulate delaminations and the 3D-Hashin failure criteria were used to predict the in-plane damage.Damage area of laminates with no boundary stress is the large,these with two opposite stress faces are intermediate,and those with one stress faces and three stress faces are the small.The residual velocity remains unchanged and the damage area increases first and then decreases when the impact velocity keeps invariable but the boundary stress increases.On the other hand the residual velocity increases linearly and damage area first increases and then decreases when impact velocity increases and boundary stress keeps constant." @default.
- W2373754471 created "2016-06-24" @default.
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- W2373754471 date "2013-01-01" @default.
- W2373754471 modified "2023-09-29" @default.
- W2373754471 title "Numerical Simulation of High Speed Impact Damage Dependence on Boundary Condition in Fiber Reinforced Laminated Composite" @default.
- W2373754471 hasPublicationYear "2013" @default.
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