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机译:Numerical simulation of the interaction between shock train and combustion in three-dimensional M12-02 scramjet model
Xi An Jiao Tong Univ, Sch Aerosp, State Key Lab Strength & Vibrat Mech Struct, Shaanxi Engn Lab Vibrat Control Aerosp Struct, Xian 710049, Peoples R China;
China Aerodynam Res & Dev Ctr, Mianyang 621000, Sichuan, Peoples R China;
Hypersonic scramjet engine; Operation performance; Shock train and combustion interaction;