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The hole in the joint or composite panel has potential to reduce the strength of the material [9], the hole in this panel becomes a reference to the progressive failure model of each ply in composite laminate, when the part experiences tensile loads, compression or shear due to moment and torque for...
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Main Author: | SOLIHAT (NIM: 23616014), AAT |
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Format: | Theses |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/24883 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
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