Three-dimensional time-marching aeroelastic analyses using an unstructured-grid Euler method
- 1 September 1993
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 31 (9), 1626-1633
- https://doi.org/10.2514/3.11824
Abstract
No abstract availableThis publication has 25 references indexed in Scilit:
- Navier-Stokes computations on swept-tapered wings, including flexibilityJournal of Aircraft, 1992
- Vortical flow computations on swept flexible wings using Navier-Stokes equationsAIAA Journal, 1990
- Technique for the prediction of airfoil flutter characteristics in separated flowJournal of Aircraft, 1989
- Unsteady transonic flow calculations for realistic aircraft configurationsJournal of Aircraft, 1989
- The effects of rotational flow, viscosity, thickness, and shape on transonic flutter dip phenomenaPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Nonlinear aspects of the transonic aeroelastic stability problemPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Unsteady full potential aeroelastic computations for flexible configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Transonic flutter analysis using the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Nonlinear transonic flutter analysisAIAA Journal, 1982