Euler flutter analysis of airfoils using unstructured dynamic meshes
- 3 April 1989
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 12 references indexed in Scilit:
- Unsteady Euler airfoil solutions using unstructured dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Finite element Euler computations in three dimensionsInternational Journal for Numerical Methods in Engineering, 1988
- Time-accurate unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Extension and applications of flux-vector splitting to unsteady calculations on dynamic meshesPublished 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
- Unsteady transonic flow calculations for realistic aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Multigrid solution of the two-dimensional Euler equations of unstructured triangular meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Calculation of Inviscid Transonic Flow over a Complete AircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- An exploratory study of finite difference grids for transonic unsteady aerodynamicsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Nonlinear transonic flutter analysisAIAA Journal, 1982