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:
| 主要作者: | |
|---|---|
| 格式: | Final Project |
| 語言: | Indonesia |
| 在線閱讀: | https://digilib.itb.ac.id/gdl/view/20816 |
| 標簽: |
添加標簽
沒有標簽, 成為第一個標記此記錄!
|