1. Chu J, Luckring JM (1996) Experimental surface pressure data obtained on 65° delta wing across Reynolds number and Mach number ranges, NASA TM 4645
2. Engler RH, Hartmann K, Troyanovski I, Vollan A (1992) Description and assessment of a new optical pressure measurement system (OPMS) demonstrated in the high speed wind tunnel of DLR in Göttingen, DLR FB 92 24
3. Hummel D (2004) Effects of boundary layer formation on the vortical flow above Slender Delta Wings, RTO specialists’ meeting on enhancement of NATO military flight vehicle performance by management of interacting boundary layer transition and separation, Prague, Czech Republic, 4–7 October 2004, Meeting Proceedings RTO-MP-AVT-111, pp 30–1 to 30–22
4. Hummel D (2005) The second international vortex flow experiment (VFE-2)––Objectives and first results. In: Proceedings of the 2nd international symposium on integrating CFD and experiments in aerodynamics, Cranfield University, Shrivenham, 5–6 September, pp 1–12
5. Hummel D, Redeker G (2003) A new vortex flow experiment for computer code validation, RTO AVT symposium on vortex flow and high angle of attack aerodynamics, Loen, 7–11 May 2001, Meeting Proceedings RTO-MP-069 (I), SYA 8–1 to 8–31