STRESS ANALYSIS OF CN 235 OUTER WINGBOX STRUCTURE USING FINITE ELEMENT METHODS
The finite element method has been used in many areas, including in the process of designing and testing aircraft structures. This method has been developed into software that is easier to use. This method uses small elements consisting of nodal to describe objects to be modeled so that objects with...
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Main Author: | (NIM: 13611058), WALIYATALATOP |
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Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/24678 |
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Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
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