TOPOLOGY OPTIMIZATION AND DAMAGE TOLERANCE ANALYSIS OF N-219 AIRCRAFT WING AND FUSELAGE FITTING

Improving performance of the N-219 aircraft that made by PT Dirgantara Indonesia must be done along with the increasing need for aircraft as a means of transportation to connect the islands in Indonesia. One thing that can be done to improve the performance of N-219 aircraft is to reduce the weight...

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Bibliographic Details
Main Author: Faruq Al Jamal, Muhamad
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/49080
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Institution: Institut Teknologi Bandung
Language: Indonesia