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Published on: January 6, 2023
Numerical Investigations of Perforated CFRP Z-Cross-Section Profiles, under Axial Compression
1Department of Machine Design and Mechatronics, Faculty of Mechanical Engineering, Lublin University of Technology, Nadbystrzycka 36, 20-618 Lublin, Poland.
Investigating perforated thin-walled composite Z-sections under compression reveals that optimized hole placement can prevent strength loss. These structures maintain stability even after buckling, crucial for aerospace and construction.
Area of Science:
- Structural Engineering
- Materials Science
- Aerospace Engineering
Background:
- Thin-walled elements are vital in aerospace and construction.
- Perforations reduce weight but alter stress distribution and stiffness.
- Understanding buckling behavior of perforated structures is critical.
Purpose of the Study:
- To numerically investigate the buckling and postbuckling behavior of thin-walled composite Z-section profiles with perforations.
- To analyze the influence of cut-out parameters (size, location, shape, number) on structural performance.
- To compare the behavior of perforated profiles with non-perforated ones.
Main Methods:
- Finite Element Method (FEM) analysis using ABAQUS® software.
- Numerical simulation of thin-walled composite Z-sections under compression.
- Evaluation of buckling load, postbuckling equilibrium path, and failure load.
Main Results:
- Perforated Z-section profiles demonstrated stable post-critical behavior.
- Optimized hole arrangement can mitigate the negative impact of perforations on mechanical properties.
- Buckling load and failure load are significantly influenced by cut-out geometry and location.
Conclusions:
- Thin-walled perforated composite Z-sections can maintain stability in the post-buckling range.
- Strategic design of cut-outs is key to preserving structural integrity and preventing performance degradation.
- Numerical analysis provides valuable insights into the complex behavior of these engineered components.
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