1. Houtman EM, Bannink WJ. Experimental investigation of the transonic flow at the leeward side of a delta wing at high incidence. TU Delft Report, LR-518, 1987
2. Elsenaar A, Hoeijmakers HW. An experimental study of the flow over a sharp-edged delta wing at subsonic speeds. AGARD CP-494, Paper no. 15, 1990
3. Hitzel SM. Wing vortex flows up into vortex breakdown—A numerical simulation. AIAA Paper, 88-2518. 1988
4. Hoeijmakers HWM, Jacobs JMJW, Van Den Berg JI. Numerical simulation of vortical flow over a delta wing at subsonic and transonic speeds. 17th ICAS, Paper No. 90-3.3.3, 1990
5. Compressible inviscid vortex flow of a sharp edge delta wing;Longo;AIAA Journal,1995