PROGRESSIVE DAMAGE ANALYSIS ON OPEN HOLE LAMINATED CFRP COMPOSITE PLATE WITH VARIOUS CONFIGURATIONS DUE TO COMPRESSION LOAD

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, Aat
Format: Theses
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/35020
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Institution: Institut Teknologi Bandung
Language: Indonesia
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