Funder
National Natural Science Foundation of China
National Key Research and Development Program of China
National University of Defense Technology
Natural Science Foundation of Hunan Province
Reference28 articles.
1. An experimental study of the effects of different transverse trenches on deposition on a turbine vane with film-cooling at high temperature;Liu;Aerosp. Sci. Technol.,2020
2. Effects of combustion on supersonic film cooling using gaseous hydrocarbon fuel as coolant;Jing-Ying;Aerosp. Sci. Technol.,2020
3. The heat dissipation, transport and reuse management for hypersonic vehicles based on regenerative cooling and thermoelectric conversion;Jian-Jun;Aerosp. Sci. Technol.,2020
4. Experimental study on supersonic film cooling on the surface of a blunt body in hypersonic flow;Fu;Chin. Phys. B,2014
5. Boundary-layer separation detection for a cone at high angle of attack in Mach 4.5 flow with pressure-sensitive paint;Running,2017
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