Buckling Analysis and Configuration Optimum Design of Grid-Stiffened Composite Panels
Author:
Affiliation:
1. Beihang University, 100191 Beijing, People’s Republic of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference25 articles.
1. Anisogrid composite lattice structures for spacecraft and aircraft applications
2. A study on grid-stiffened multi-functional composite structures with radiation spot shielding
3. Design, analysis, fabrication, and testing of composite grid-stiffened panels for aircraft structures
4. Hybrid analysis and optimization of hierarchical stiffened plates based on asymptotic homogenization method
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