Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures
Auteur(s): |
Nabil M. Chowdhury
John Wang Wing Kong Chiu Paul Chang |
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Médium: | article de revue |
Langue(s): | anglais |
Publié dans: | Composite Structures, mai 2016, v. 142 |
Page(s): | 96-106 |
DOI: | 10.1016/j.compstruct.2016.01.078 |
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10452945 - Publié(e) le:
23.10.2020 - Modifié(e) le:
23.10.2020