Applications of a fast, time accurate full potential scheme to a statically flexible wing in the transonic regime
- 6 April 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- TREATMENT OF STEADY AND UNSTEADY FLOWS USING A FAST TIME-ACCURATE FULL POTENTIAL SCHEMEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A UNIFIED FULL POTENTIAL SCHEME FOR SUBSONIC, TRANSONIC, AND SUPERSONIC FLOWSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A fast, time-accurate unsteady full potential schemePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Unsteady aerodynamic modeling of a fighter wing in transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- An alternating-direction implicit algorithm for unsteady potential flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- A CONSERVATIVE IMPLICIT FINITE DIFFERENCE ALGORITHEM FOR THE UNSTEADY TRANSONIC FULL POTENTIAL EQUATIONPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980