Numerical investigation of vortex breakdown on a delta wing

S Agrawal, RM Barnett, BA Robinson - AIAA journal, 1992 - arc.aiaa.org
A numerical investigation of leading-edge vortex breakdown on a delta wing at high angles
of attack is presented. The analysis has been restricted to low-speed flows on a flat-plate …
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[引用][C] Numerical investigation of vortex breakdown on a delta wing

S Agrawal, RM Barnett, BA Robinson - AIAA Journal, 1992 - ui.adsabs.harvard.edu
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[引用][C] Numerical investigation of vortex breakdown on a delta wing

S AGRAWAL, RM BARNETT, BA ROBINSON - AIAA journal, 1992 - pascal-francis.inist.fr
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[引用][C] Numerical investigation of vortex breakdown on a delta wing

S AGRAWAL, RM BARNETT… - AIAA …, 1992 - American Institute of Aeronautics …