A multiblock approach to solving the three-dimensional unsteady Euler equations about a wing-pylon-store configuration
- 14 August 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- A composite grid generation code for general 3-D regionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Multigrid acceleration of the flux split Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Characteristic-Based Schemes for the Euler EquationsAnnual Review of Fluid Mechanics, 1986
- A 3-D chimera grid embedding techniquePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A new class of high accuracy TVD schemes for hyperbolic conservationlawsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Application of a new class of high accuracy TVD schemes to the Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- A conservative treatment of zonal boundaries for Euler equation calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Approximate Riemann solvers, parameter vectors, and difference schemesJournal of Computational Physics, 1981
- Flux vector splitting of the inviscid gasdynamic equations with application to finite-difference methodsJournal of Computational Physics, 1981
- Towards the ultimate conservative difference scheme. II. Monotonicity and conservation combined in a second-order schemeJournal of Computational Physics, 1974