Funder
Science Foundation of the National University of Defense Technology
Foundation of the National University of Defense Technology
National Natural Science Foundation of China
Reference23 articles.
1. Numerical and experimental study on waverider with blunt leading edge;Liu;Comput. Fluids,2013
2. Forward facing spike effects of bodied of different cross section in supersonic flow;Hutt;Aeronaut. J.,1989
3. Numerical investigation of supersonic flows around a spiked blunt body;Yamauehi;J. Spacecr. Rockets,1995
4. Effect of pressure ratio on aerodynamic heating reduction due to opposing jet;Hayashi,2003
5. Aerodynamic drag reduction by plasma and hot-gas injection;Ganiev;J. Thermophys. Heat Transf.,2000
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