Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows
Author:
Affiliation:
1. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.867
Reference34 articles.
1. On the use of Pade approximants to represent unsteady aerodynamic loads for arbitrarily small motions of wings
2. Applications of Laplace transform methods to airfoil motion and stability calculations
3. Design for Active Flutter Suppression and Gust Alleviation Using State-Space Aeroelastic Modeling
4. Eigenanalysis of unsteady flows about airfoils, cascades, and wings
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