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Communication Dans Un Congrès Année : 2011

Impacts on fuselages: a trial in using numerical simulation to predict residual strength

Frederic Lachaud
Christine Espinosa
Laurent Michel
Michel Salaün

Résumé

Quasi-static and dynamic characterization tests laminates have been carried out on balanced angle ply [±θ] and used for calibration of numerical values of different models derived to predict damage initiation and growth in aeronautical large structures. Impact induced damage from experiment’s measures and numerical predictions are compared for T800/M21S aeronautical samples impacted at 15J.
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Dates et versions

hal-02191639 , version 1 (23-07-2019)

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  • HAL Id : hal-02191639 , version 1

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Frederic Lachaud, Christine Espinosa, Laurent Michel, Michel Salaün. Impacts on fuselages: a trial in using numerical simulation to predict residual strength. Workshop on "Dynamic Failure of Composite and Sandwich Structures", 23-24 June 2011, ICA, Toulouse (FR), 2011, Toulouse, France. ⟨hal-02191639⟩
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