Computations of viscous flows for multi-element wings using hybrid structured-unstructured grids
- 6 January 1997
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Development of a 3-D zonal implicit procedure for hybrid structured-unstructured gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1996
- Navier-Stokes analysis of the flow about a flap edgePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- Viscous unstructured three-dimensional grids by the advancing-layers methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Recent progress toward a three-dimensional unstructured Navier-Stokes flow solverPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1994
- Structured background grids for generation of unstructured grids by advancing-front methodAIAA Journal, 1993
- Solution of the 2D Navier-Stokes equations on unstructured adaptive gridsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Adaptive remeshing for compressible flow computationsJournal of Computational Physics, 1987
- An LU-SSOR scheme for the Euler and Navier-Stokes equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Computing Dirichlet Tessellations in the PlaneThe Computer Journal, 1978