Dynamic Optimization of Buckling Problems for Panel Structures with Stiffening Characteristics
Many kinds of panel structures are proposed in aircraft design. This study presents a topology optimization method to improve the buckling resistance of panel structures. It should be noted that a popular configuration of the present panel structure is that with ribs and frames. Stiffening character...
Saved in:
| Main Authors: | Yuguang Bai, Xiangmian He, Qi Deng, Dan Zhao |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2025-07-01
|
| Series: | Applied Sciences |
| Subjects: | |
| Online Access: | https://www.mdpi.com/2076-3417/15/15/8227 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel
by: Ouadia Mouhat, et al.
Published: (2019-08-01) -
Finite Element Analysis of Post-Buckling Failure in Stiffened Panels: A Comparative Approach
by: Jakiya Sultana, et al.
Published: (2025-04-01) -
Nonlinear static and dynamic buckling of eccentrically stiffened functionally graded cylindrical shells under axial compression surrounded by an elastic foundation
by: Vu Hoai Nam, et al.
Published: (2014-02-01) -
Review on integral stiffened panel of aircraft fuselage structure
by: Devi Chandra, et al.
Published: (2025-04-01) -
Nonlinear buckling and post-buckling of eccentrically stiffened functionally graded cylindrical shells surrounded by an elastic medium based on the first order shear deformation theory
by: Dao Van Dung, et al.
Published: (2013-11-01)