Flow simulations using Euler equations for nacelle-propeller configurations in a wind tunnel environment
- 16 July 1985
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Flow simulations for nacelle-propeller configurations using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Finite volume calculation of three-dimensional potential flow arounda propellerAIAA Journal, 1983
- Flow simulations for general nacelle configurations using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Transfinite mesh generation and damped Euler equation algorithm for transonic flow around wing-body configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Body-fitted 3-D full-potential flow analysis of complex ducts and inletsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Transonic potential flow computation about three-dimensional inlets,ducts and bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980