Computation of the flutter boundary of an airfoil with a parallel Navier-Stokes solver
Author:
Affiliation:
1. CERFACS, Toulouse, France
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-572
Reference34 articles.
1. On the Transonic-Dip Mechanism of Flutter of a Sweptback Wing
2. Approximate Riemann solvers, parameter vectors, and difference schemes
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