Algorithm for Compression Design Allowable Determination of Composite Laminates with Initial Delaminations
With the increasing demands for detailed design of composite aircraft structures, the method of covering all damages with low design allowables cannot meet the current requirements for aircraft structure design. Herein, this paper proposes a novel algorithm for design allowable determination of comp...
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| Autors principals: | , , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
MDPI AG
2021-11-01
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| Col·lecció: | Machines |
| Matèries: | |
| Accés en línia: | https://www.mdpi.com/2075-1702/9/12/307 |
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