An efficient procedure for flutter boundary prediction on parallel computers
- 10 April 1995
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Parallel computation of 3-D Navier-Stokes flowfields for supersonic vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- An exploratory study of finite difference grids for transonic unsteady aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- COMPARISON OF SUPERCRITICAL AND CONVENTIONAL WING FLUTTER CHARACTERISTICSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1976