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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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Bibliographic Details
Main Author: SOLIHAT (NIM: 23616014), AAT
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/24883
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Institution: Institut Teknologi Bandung
Language: Indonesia