STRUCTURAL STRENGTH ANALYSIS OF COMPOSITE BLADE STIFFENED PANEL UNDER PULL-OUT TENSILE LOADING USING FINITE ELEMENT METHOD AND EXPERIMENTAL

Composite blade stiffened panels are structures that are widely used in aircraft structures such as wings and fuselage. Generally, the stiffener installation on the panel aims to add stiffeness so that the structure is more rigid, strong but light weight. Finding out the strength of the blade stiffe...

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Bibliographic Details
Main Author: Handoko
Format: Theses
Language:Indonesia
Subjects:
Online Access:https://digilib.itb.ac.id/gdl/view/47415
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Institution: Institut Teknologi Bandung
Language: Indonesia

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