Thermal Buckling Analysis and Optimization of Curvilinearly Stiffened Plates with Variable Angle Tow Laminates
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34378
Reference47 articles.
1. Thermal Buckling of Plates and Shells
2. STIFFNESS, THERMAL EXPANSION, AND THERMAL BENDING FORMULATION OF STIFFENED, FIBER-REINFORCED COMPOSITE PANELS
3. Design and Evaluation of a Reinforced Advanced-Grid Stiffened Composite Structure
4. High Temperature Composite Materials
5. Tow-Placement Technology and Fabrication Issues for Laminated Composite Structures
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