Grid generation and transonic flow calculations for three-dimensional configurations
Author:
- 14 July 1980
- conference paper
- 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 winglets1980
- Direct control of the grid point distribution in meshes generated by elliptic equationsfor solution of Navier-Stokes nozzle flow1979
- Computational transonic flow about realistic aircraft configurations1978
- A finite volume method for transonic potential flow calculations1977
- Automatic numerical generation of body-fitted curvilinear coordinate system for field containing any number of arbitrary two-dimensional bodiesJournal of Computational Physics, 1974