Simulation of static and dynamic aeroelastic behavior of a flexible wing with multiple control surfaces
- 2 April 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- An effective flutter control method using fast, time-accurate CFD codesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Unsteady full potential aeroelastic computations for flexible configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Applications of a fast, time accurate full potential scheme to a statically flexible wing in the transonic regimePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- 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
- 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