Aeroelastic analysis of an airfoil using eigenmode based reduced order unsteady aerodynamics
- 10 April 1995
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- A Reduced Order Model of Unsteady Flows in TurbomachineryPublished by ASME International ,1994
- Eigenvalue calculation procedure for an Euler/Navier-Stokes solver with application to flows over airfoilsJournal of Computational Physics, 1991
- Role of artificial viscosity in Euler and Navier-Stokes solversAIAA Journal, 1991