Buckling Analysis of Airframe Jointed Panel Under Combined Loading
The complicated relationship of the high order static indeterminate structure will lead to a lot of calculation work. The strength analysis of the structure is very difficult. In aircraft design phase, a structural simplified method should be used to model the load characteristics of the structure....
| الحاوية / القاعدة: | International Journal of Applied Mechanics and Engineering |
|---|---|
| المؤلفون الرئيسيون: | , , |
| التنسيق: | مقال |
| اللغة: | الإنجليزية |
| منشور في: |
University of Zielona Góra
2018-11-01
|
| الموضوعات: | |
| الوصول للمادة أونلاين: | https://www.ijame-poland.com/Buckling-Analysis-of-Airframe-Jointed-Panel-Under-Combined-Loading,166960,0,2.html |