Zonal Navier-Stokes methodology for flow simulation about a completeaircraft
- 1 July 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 27 (7) , 583-590
- https://doi.org/10.2514/3.25326
Abstract
No abstract availableKeywords
This publication has 16 references indexed in Scilit:
- Simulation of transonic viscous flow over a fighter-like configuration including inletPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Transonic Navier-Stokes solutions for a fighter-like configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Improvements to the aircraft Euler methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- A numerical investigation on wing/nacelle interferences of USB configurationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Flow simulations for a complex airplane configuration using Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Numerical optimization design of advanced transonic wing configurationsPublished 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
- A zonal approach to solution of the Euler equationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- A grid interfacing zonal algorithm for three-dimensional transonic flows about aircraft configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Component-adaptive grid interfacingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981