1. Barth TJ, Jespersen D (1989). The Design and Application of Upwind Schemes on Unstructured Meshes. Technical Report AIAA-89–0366.AIAA 27th Aerospace Sciences Meeting, Reno.
2. Chiba K, Obayashi S, Kazuhiro K (2004). CFD Visualization of Second Primary Vortex Structure on a 65-Degree Delta Wing. AIAA 2004–5378.22nd Applied Aerodynamics Conference and Exhibit, 16–19 August 2004, Providence, Rhode Island.
3. Chu J, Luckring JM (1996a).Experimental Surface Pressure Data Obtained on a 65°Delta Wing across Reynolds Number and Mach Number Ranges. Volume 1—Sharp Leading Edge. NASA TM-4645.
4. Chu J, Luckring JM (1996b).Experimental Surface Pressure Data Obtained on a 65°Delta Wing across Reynolds Number and Mach Number Ranges. Volume 2—Medium Leading Edge. NASA TM-4645.
5. Crippa S, Rizzi A (2006). Numerical Investigation of Reynolds Number Effects on a Blunt Leading-Edge Delta Wing. AIAA 2006–3001.24th AIAA Applied Aerodynamics Conference, June 5–8 2006, San Francisco, California.