RESEARCH OF ANALYTICAL DETERMINISTIC METHOD MULTIPLE SITE DAMAGE CASE WITH STIFFENERS EFFECT WITH COMPOUNDING METHOD
Crack flaw is one of the common cause in the structural failure of aircraft, especially on skin and plate of fuselage and wing. Multiple Site Damage (MSD) can occur when this crack flaw is on the part of the structure with array of holes. MSD can cause a significant decrease in residual strength of...
Saved in:
Main Author: | Domas Indrawijaya - Nim: 13613049, Agus |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/20816 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Similar Items
-
STUDI METODE ANALISIS DETERMINISTIK KASUS MULTIPLE SITE DAMAGE DENGAN PENGARUH INTERAKSI STIFFENER MENGGUNAKAN METODE COMPOUNDING
by: Domas I, Agus -
COMPOSITE LAMINATE STACKING SEQUENCE FOR WEIGHT AND BUCKLING LOAD OPTIMIZATION OF STIFFENED PANEL STRUCTURE
by: Domas Indrawijaya, Agus -
DAMAGE TOLERANCE ANALYSIS FOR MULTIPLE SITE DAMAGE LAP JOINT FUSELAGE CN 235 WITH PROBABILISTIC METHOD
by: EDY PRASETYO (NIM : 23607025); Pembimbing 1 : Prof. Dr. Ichsan Setya Putra; Pembimbing 2 : Dr, EKO -
EVALUATION OF STRESS INTENSITY FACTOR OF MULTIPLE SITE DAMAGE CRACKS USING BOUNDARY ELEMENT METHOD
by: YULLYAWAN (NIM : 23607007); Pembimbing : Dr. Ir. Ichsan Setya Putra; Dr. Ir. Tatacipta Dir, ANDHI -
DEVELOPMENT OF MULTIPLE SITE DAMAGE PROBABILISTIC ANALYSIS OF AGING AIRCRAFT USING BOUNDARY ELEMENT METHOD
by: INDRIYANI SIBARANI, INTAN