Convergence acceleration of a Navier-Stokes solver for efficient static aeroelastic computations
- 1 June 1995
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 33 (6) , 1134-1141
- https://doi.org/10.2514/3.12533
Abstract
No abstract availableThis publication has 18 references indexed in Scilit:
- Navier-Stokes computations for oscillating control surfacesJournal of Aircraft, 1994
- Fluid-structural interactions using Navier-Stokes flow equations coupled with shell finite element structuresPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1993
- Unsteady shock-vortex interaction on a flexible delta wingJournal of Aircraft, 1992
- Streamwise upwind algorithm for computing unsteady transonic flows past oscillating wingsAIAA Journal, 1991
- On Godunov-type methods near low densitiesJournal of Computational Physics, 1991
- Ensaero—A multidisciplinary program for fluid/structural interaction studies of aerospace vehiclesComputing Systems in Engineering, 1990
- Upwind algorithms for general thermo-chemical nonequilibrium flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Lower-upper Symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equationsAIAA Journal, 1988
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- Thin-layer approximation and algebraic model for separated turbulentflowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978