2019•International Journal of CrashworthinessRequires access

Damage and residual compressive strength of multi-layer composite laminates after low velocity impact

Fangyu Chen, Zhou Li, Tang Yihao

Open publisher page 12 citations

Abstract

In this article, an integrated analytical model is built to predict the damage and compressive strength of multi-layer composite laminates after low velocity impact (CAI). First, the low velocity impact process and the impact damage are simulated. Then, the state of damage is taken as the input for analysing the residual compressive strength. In order to validate these analytical studies, three kinds of multi-layer composite laminates mixed-formed by uni-directional layer HS160SF and woven layer HS220DF are tested good agreements between simulative and experimental results are obtained.

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What this paper is about

In this article, an integrated analytical model is built to predict the damage and compressive strength of multi-layer composite laminates after low velocity impact (CAI). First, the low velocity impact process and the impact damage are simulated. Then, the state of damage is taken as the input for analysing the residual compressive strength. In order to validate these analytical studies, three kinds of multi-layer composite laminates mixed-formed by uni-directional layer HS160SF and woven layer HS220DF are tested good agreements between simulative and experimental results are obtained.

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OpenAlex reports 12 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

In this article, an integrated analytical model is built to predict the damage and compressive strength of multi-layer composite laminates after low velocity impact (CAI). First, the low velocity impact process and the impact damage are simulated. Then, the state of damage is taken as the input for analysing the residual compressive strength. In order to validate these analytical studies, three kinds of multi-layer composite laminates mixed-formed by uni-directional layer HS160SF and woven layer HS220DF are tested good agreements between simulative and experimental results are obtained.

Key concepts: Materials science, Composite number, Composite material, Residual, Compressive strength, Residual strength, Composite laminates, Layer (electronics)

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