Ozawa H, Laurence SJ (2018) Experimental Investigation of the Shock-Induced Flow over a Wall-Mounted Cylinder, J. Fluid. Mech., Vol.849, pp.1009-1042.
Laurence SJ, Ozawa H, Schramm JM, Hannemann K (2019) Heat-flux and combustion measurements on a Hypersonic intake ramp using fast-response temperature sensitive paint, Exp. Fluids., 60(4):70.
Ozawa H and Laurence SJ (2018) A Transient Global Heat-Flux Measurements for High-Speed Flow over a Wall-Mounted Cylinder in a Shock Tube, 22nd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 17-19, September, 2018, AIAA-2018-5384.
Laurence SJ, Ozawa H, Schramm JM, and Hanneman K (2018) Fast-response temperature sensitive paint measurements on a hypersonic inlet ramp, 22nd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 17-19, September, 2018, AIAA-2018-5383.
Schramm JM, Karl S, Hannemann K and Ozawa H (2018) Ultra-fast Temperature Sensitive Paint Shock Tunnel Heat Flux Measurements on the Intake of the LAPCAT II Small Scale Flight Experiment Configureation, HiSST: International Conference on High-Speed Vehicle Science Technology, 26-29 November 2018, Moscow, Russia.
Ozawa H (2018) Experimental Investigation of Nonstationary High-Speed Flow over a Wall-Mounted Cylinder using TSP, 12th International Workshop on Shock Tube Technology, IWSTT, Kakuda Space Center, 12-13, April, 2018.
Schramm JM, Ozawa H, Hannemann K, Hilfer M, Klein C, Edzards F, Jauch J, Mee D (2018) Ultra-fast Temperature Sensitive Paints (TSP) in the High Enthalpy Shock Tunnel Göttingen, HEG, 12th International Workshop on Shock Tube Technology, IWSTT, Kakuda Space Center, 12-13, April, 2018.
