Discrete element approach to flutter of skew panels with in-plane forces under yawed supersonic flow
Author:
Affiliation:
1. National Aeronautical Laboratory, Bangalore, India
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.6040
Reference12 articles.
1. Flutter of Rectangular Simply Supported Panels at High Supersonic Speeds
2. Flutter of Thin Plates under Combined Shear and Normal Edge Forces
3. Application of matrix displacement methods in the study of panel flutter.
4. Argyris, J. H. "Matrix Displacement Analysis of Plates and Shells/' Ingenieur-Archiv, XXXV Band 1966.
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