Aeroelastic Stability and Nonlinear Flutter Analysis of Heated Panel with Temperature-Dependent Material Properties
Author:
Affiliation:
1. Ph.D. Candidate, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.
2. Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author).
Publisher
American Society of Civil Engineers (ASCE)
Subject
Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering
Link
http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001173
Reference38 articles.
1. SECONDARY BIFURCATIONS AND GLOBAL INSTABILITY OF AN AEROELASTIC NON-LINEAR SYSTEM IN THE DIVERGENCE DOMAIN
2. Hopf Bifurcation of Heated Panels Flutter in Supersonic Flow
3. Nonlinear vibrations, bifurcations and chaos of lattice sandwich composite panels on Winkler–Pasternak elastic foundations with thermal effects in supersonic airflow
4. Aerothermoelastic flutter analysis and active vibration suppression of nonlinear composite laminated panels with time-dependent boundary conditions in supersonic airflow
5. Active aerothermoelastic flutter suppression of composite laminated panels with time-dependent boundaries
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