Unsteady full potential aeroelastic computations for flexible configurations
- 8 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- 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
- Transonic aeroelastic analysis of the B-1 wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Entropy condition satisfying approximations for the full potential equation of transonic flowMathematics of Computation, 1985
- Unsteady aerodynamic modeling of a fighter wing in transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Some recent applications of XTRAN3SPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Flutter analysis of a transport wing using XTRAN3SPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Comparison between computations and experimental data in unsteady three-dimensional transonic aerodynamics, including aeroelastic applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982