Comparison between Rivet and Adhesive joints in Center Wingbox using Finite Element Method
Composite materials are used extensively as aircraft structures due to their design flexibility to create a light weight, high stiffness, and high ultimate stress structure. These structures are usually joined by using rivet joint because its simplicity and easiness for dissasembly. However, a study...
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| Format: | Final Project |
| Language: | Indonesia |
| Online Access: | https://digilib.itb.ac.id/gdl/view/23203 |
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| Institution: | Institut Teknologi Bandung |
| Language: | Indonesia |