Finite Element and Machine Learning-Based Prediction of Buckling Strength in Additively Manufactured Lattice Stiffened Panels
The current research aimed to investigate the critical buckling load of a simply supported aerospace-grade stiffened panel made of additively manufactured cubic lattice unit cell arrays, namely simple cubic, face-centered cubic (FCC) and body-centered cubic (BCC) structures. Ansys Design Modeler was...
Saved in:
Main Authors: | Saiaf Bin Rayhan, Md Mazedur Rahman, Jakiya Sultana, Szabolcs Szávai, Gyula Varga |
---|---|
Format: | Article |
Language: | English |
Published: |
MDPI AG
2025-01-01
|
Series: | Metals |
Subjects: | |
Online Access: | https://www.mdpi.com/2075-4701/15/1/81 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
APPLICABILITY INVESTIGATION OF FAILURE CRITERION FOR POST-BUCKLING ANALYSIS OF STIFFENED COMPOSITE PANELS
by: LIN GuoWei, et al.
Published: (2020-01-01) -
Adaptive Spatial Lattice Manufacturing (ASLM): A novel approach to efficient lattice structure production
by: Justin Dirrenberger, et al.
Published: (2025-01-01) -
Metallic perforated plate lattices with superior buckling strength
by: Lei Zhang, et al.
Published: (2025-01-01) -
STIFFENER-SKIN INTERFACE FAILURE CHARACTERIZATION OF THE STIFFENED COMPOSITE PANEL AT POST-BUCKLING STAGE
by: HU BoTao, et al.
Published: (2019-01-01) -
The Effects of Ply Orientation on Nonlinear Buckling of Aircraft composite Stiffened Panel
by: Ouadia Mouhat, et al.
Published: (2019-08-01)