Vibration Analysis of Curvilinearly Stiffened Composite Panel Subjected to In-Plane Loads
Author:
Affiliation:
1. Virginia Polytechnic Institute and State University, Blacksburg, Virginia 24061
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J055047
Reference34 articles.
1. Future of Flight Vehicle Structures (2000 to 2023)
2. Flight Vehicle Composite Structures
3. Status of Advanced Stitched Unitized Composite Aircraft Structures
4. Optimal Design of Unitized Panels with Curvilinear Stiffeners
5. Wing-Box Weight Optimization Using Curvilinear Spars and Ribs (SpaRibs)
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