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The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. III: Computational predictions of the NIST multiple site damage experimental results - MaRDI portal

The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. III: Computational predictions of the NIST multiple site damage experimental results (Q1365780)

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scientific article; zbMATH DE number 1058790
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English
The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. III: Computational predictions of the NIST multiple site damage experimental results
scientific article; zbMATH DE number 1058790

    Statements

    The elastic-plastic finite element alternating method (EPFEAM) and the prediction of fracture under WFD conditions in aircraft structures. III: Computational predictions of the NIST multiple site damage experimental results (English)
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    9 September 1997
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    A series of predictions are compared with experimental data to validate the model for computing the residual strength under wide spread fatigue damage conditions. The worst prediction differs about \(15\%\) from the experiment.
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    residual strength
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    fatigue damage conditions
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