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...
Saved in:
Main Author: | |
---|---|
Format: | Theses |
Language: | Indonesia |
Subjects: | |
Online Access: | https://digilib.itb.ac.id/gdl/view/47415 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |