Combined loadings after medium velocity impact on large CFRP laminated plates: Discrete ply model simulations
To decrease development costs of aeronautical composite structures, industrials and academic researchers are turning to “virtual testing” methods. To help achieve this objective, a new methodology has been developed at the Institut Clément Ader. It is based on a complex loading test rig for technolo...
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Autores principales: | , , , , , |
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Formato: | article |
Lenguaje: | EN |
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Elsevier
2021
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Acceso en línea: | https://doaj.org/article/e5255202a6b4463c8c1eaa8724b61e56 |
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