1. Y. Iijima et al. ”Optimization of Temperature-Sensitive Paint Formulation for Large-Scale Cryogenic Wind Tunnels”, In 20 International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF). Göttingen, Germany, August 25.-29., 2003, pp 70–77.
2. U. Fey et al. ”Transition Detection by Temperature Sensitive Paint at Cryogenic Temperatures in the European Transonic Windtunnel (ETW)”, 20 International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF). Gottingen, Germany, August 25.-29., 2003, pp. 77–88.
3. U. Fey, Y. Egami, and R.H. Engler: ”High Reynolds Number Transition Detection by Means of Temperature Sensitive Paint”, In 44th AIAA Aerospace Sciences Meeting and Exhibit. Reno, NV, USA 2006, AIAA 2006–2514.
4. Y. Egami, U. Fey, Ch. Klein, M. Sitzmann and J. Wild. ”Transition Detection on High-lift Devices in DNW-KKK by means of Temperature-Sensitive Paint”. In 12th International Symposium on Flow Visualization. Göttingen, Germany, September 10–14, 2006.
5. M. Drela and M.B. Giles: ”Viscous-Inviscid Analysis of Transonic and Low Reynolds Number Airfoils”, AIAAA Journal 25(10), October 1987, pp. 1347–1355.