EFFECTS OF ORTHOTROPICITY ORIENTATION ON SUPERSONIC PANEL FLUTTER
Author:
Affiliation:
1. Massachusetts Institute of Technology, Cambridge, Mass.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2033
Reference4 articles.
1. Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds
2. An Introduction to Applied Anisotropic Elasticity
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