Transonic Navier-Stokes solutions for a fighter-like configuration
- 1 October 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (10) , 875-881
- https://doi.org/10.2514/3.45674
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Theoretical analysis of aircraft afterbody flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Numerical simulation of the tip vortex off a low-aspect-ratio wing at transonic speedPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Three-dimensional flow over a conical afterbody containing a centered propulsive jet - A numerical simulationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Computational Aerodynamics Development and OutlookAIAA Journal, 1979