Grid generation and transonic flow calculations for three-dimensional configurations
- 14 July 1980
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Simulated transonic flows for aircraft with nacelles, pylons, and wingletsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Direct control of the grid point distribution in meshes generated by elliptic equationsfor solution of Navier-Stokes nozzle flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Computational transonic flow about realistic aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- A finite volume method for transonic potential flow calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974