Static and fatigue testing bolted, bonded and hybrid step lap joints of thick carbon fibre/epoxy laminates used on aircraft structures
| Author(s): |
Nabil M. Chowdhury
John Wang Wing Kong Chiu Paul Chang |
|---|---|
| Medium: | journal article |
| Language(s): | English |
| Published in: | Composite Structures, May 2016, v. 142 |
| Page(s): | 96-106 |
| DOI: | 10.1016/j.compstruct.2016.01.078 |
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10452945 - Published on:
23/10/2020 - Last updated on:
23/10/2020
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