Implementation of a fully-implicit, aeroelastic Navier-Stokes solver
Author:
Affiliation:
1. USAF, Research Lab., Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-2039
Reference22 articles.
1. Unsteady aerodynamic and aeroelastic calculations for wings using Euler equations
2. Wing flutter computations using an aerodynamic model based on the Navier-Stokes equations
3. Alonso, J., Martinelli, L. and Jameson, A. "Multigrid Unsteady Navier-Stokes Calculations with Aeroelastic Applications," AIAA Paper 95-0048,Jan.1995.
4. Towards cost-effective aeroelastic analysis on advanced parallel computing systems
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