Panel Aeroelastic Stability in Irregular Shock Reflection
Author:
Affiliation:
1. Northwestern Polytechnical University, 710072 Xi’an, People’s Republic of China
2. Duke University, Durham, North Carolina 27708-0300
Funder
Project from the Ministry of Industry and Information Technology of China
Fundamental Research Funds for the Central Universities
Fund of NPU-Duke China Seed Program
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J061902
Reference19 articles.
1. Panel flutter - A review of the aeroelastic stability of plates and shells
2. DowellE. H., Aeroelasticity of Plates and Shells, Noordhoff International, Leyden, The Netherlands, 1975, pp. 1–9, Chap. 1.
3. Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds
4. Transonic Panel Flutter in Accelerating or Decelerating Flow Conditions
5. Nonlinear Dynamics of Prestressed Panels in Low Supersonic Turbulent Flow
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