1. K. Asai, H. Kanda, T. Kunimasu, T. Liu, J.P. Sullivan, Detection of boundary-layer transition in a cryogenic wind tunnel by using luminescent paint. AIAA Paper 96-2185, 1996
2. K. Asai, T. Kunimasu, Y. Iijima, Visualization of the quiet test region in a supersonic wind tunnel using luminescent paint, in ICIASF’97 Record, 17th International Congress on Instrumentation in Aerospace Simulation Facilities, 29 Sept–2 Oct, Pacific Grove, CA (1997b), pp. 84–94
3. K. Asai, H. Kanda, T. Kunimasu, T. Liu, J.P. Sullivan, Boundary-layer transition detection in a cryogenic wind tunnel using luminescent paint. J. Aircraft 34(1), 34–42 (1997c)
4. V. Borovoy, V. Mosharov, A. Noev, V. Radchenko, Temperature sensitive paint application for investigation of boundary layer transition in short-duration wind tunnels, in EUCASS-2009, 6–9 Jul 2009, Versailles, France (2009)
5. V. Borovoy, V. Mosharov, V. Radchenko, Surface flow visualization in short duration wind tunnel, in Proceedings of the 9th Pacific Symposium on Flow Visualization and Image Processing (PSFVIP-9), 25–28 Aug 2013, Busan, Korea (2013), pp. 125–130