Numerical study of the vortex burst phenomenon for delta wings
Author:
Affiliation:
1. Vigyan Research Associates, Inc., Hampton, VA
2. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-505
Reference22 articles.
1. [I] Proceedings of the AIAA 8th Computational
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1. Navier-Stokes Analysis of Tunnel-Wall Interference Effects on Pitching Delta Wings;Journal of Aircraft;2004-05
2. On the structure of vortex breakdown on a delta wing;Proceedings of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;1998-01-08
3. Navier-Stokes simulation of the low Mach number flows over a delta wing by an upwind NND scheme;Theroretical Fluid Mechanics Conference;1996-06-17
4. Numerical investigation of subsonic flow over a typical missile forebody;34th Aerospace Sciences Meeting and Exhibit;1996-01-15
5. Numerical prediction of vortical flow over slender delta wings;Journal of Aircraft;1993-11
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