Nonlinear Flutter Suppression and Thermal Buckling Elimination for Composite Lattice Sandwich Panels
Author:
Affiliation:
1. Harbin Institute of Technology, 150001 Harbin, People’s Republic of China
2. Harbin Engineering University, 150001 Harbin, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference51 articles.
1. Crushing of a Textile Core Sandwich Panel
2. The effects of nonlinearities on the vibration of viscoelastic sandwich plates
3. Postbuckling of sandwich plates with nanotube-reinforced composite face sheets resting on elastic foundations
4. Free Vibration of Thermally Buckled Composite Sandwich Plates
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