State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.47019
Reference15 articles.
1. Theoretical considerations of panel flutter at high supersonic Mach numbers.
2. Large-amplitude finite element flutter analysis of composite panels in hypersonic flow
3. Matrix fraction approach for finite-state aerodynamic modeling
4. State-space representation of unsteady airfoil behavior
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