Transonic Flutter Simulations Using an Implicit Aeroelastic Solver
- 1 September 2000
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 37 (5) , 872-879
- https://doi.org/10.2514/2.2683
Abstract
No abstract availableThis publication has 16 references indexed in Scilit:
- Fully implicit aeroelasticity on overset grid systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1998
- Wing flutter computations using an aerodynamic model based on the Navier-Stokes equationsJournal of Aircraft, 1996
- Numerical simulation of spiral vortex breakdown above a delta wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Computation of delta-wing roll maneuversJournal of Aircraft, 1995
- Multigrid unsteady Navier-Stokes calculations with aeroelastic applicationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Onset of vortex breakdown above a pitching delta wingAIAA Journal, 1994
- Unsteady aerodynamic and aeroelastic calculations for wings using Euler equationsAIAA Journal, 1990
- Implicit Finite-Difference Simulations of Three-Dimensional Compressible FlowAIAA Journal, 1980
- Geometric Conservation Law and Its Application to Flow Computations on Moving GridsAIAA Journal, 1979
- An Implicit Factored Scheme for the Compressible Navier-Stokes EquationsAIAA Journal, 1978