1. M. Elsayed, F. Scarano, and N. G. Verhaagen, “Leading-edge shape effect on the flow over non-slender delta wings,” AIAA Paper No. 2008-344, Reno, January 2008.
2. J. M. Luckring, “Reynolds number and leading-edge bluntness effects on a 65° delta wing,” AIAA Paper No. 2002-0419, Reno, January 2002.
3. R. M. Cummings and A. Schütte, “Detached-eddy simulation of the vortical flowfield about the VFE-2 delta wing,” AIAA Paper No. 2008-396, Reno, January 2008.
4. A. M. Mitchell, “Caractérisation et contrôle de l’éclatement tourbillonnaire sur une aile delta aux hautes incidences,” Ph.D. thesis, University Paris 6, France, 2000.
5. F. Renac, “Contrôle expérimental de l’écoulement tourbillonnaire sur une aile delta,” Ph.D. thesis, University Paris 6, France, 2004.