1. Some features of a separated flow and supersonic vortex structure at the leeside of a delta wing;Brodetsky,1991
2. The compressible inviscid lead-edge vortex;Brown;J. Fluid Mech.,1965
3. T.A. Buter, D.P. Rizzetta, Steady supersonic Navier–Stokes solutions of a 75 deg delta wing, NASA CP-2416, NASA Langley Research Center, Hampton, VA, 1985
4. A.H. Craven, A.J. Alexander, An investigation of vortex breakdown at Mach 2, CoA Note Aero-158, Cranfield College of Aeronautics, UK, 1963
5. S.R. Donohoe, Vortex flow and vortex breakdown above a delta wing in high subsonic flow: an experimental investigation, Ph.D. Dissertation, Delft University of Technology, The Netherlands, 1996