An elasticity-based mesh scheme applied to the computation of unsteady three-dimensional spoiler and aeroelastic problems
- 22 August 1999
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- Analysis of Fluid-Structure Interaction by Means of Dynamic Unstructured MeshesJournal of Fluids Engineering, 1998
- Implementation of a fully-implicit, aeroelastic Navier-Stokes solverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1997
- Comparison of the predictive capabilities of several turbulence modelsJournal of Aircraft, 1995
- Wing flutter boundary prediction using unsteady Euler aerodynamic methodJournal of Aircraft, 1995
- Static aeroelastic analysis of fighter aircraft using a three-dimensional Navier-Stokes algorithmJournal of Aircraft, 1990
- Euler flutter analysis of airfoils using unstructured dynamic meshesJournal of Aircraft, 1990
- Unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsAIAA Journal, 1990
- Modern wing flutter analysis by computational fluid dynamics methodsJournal of Aircraft, 1988
- Extension and applications of flux-vector splitting to unsteady calculations on dynamic meshesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Time-marching transonic flutter solutions including angle-of-attack effectsJournal of Aircraft, 1983