Aerodynamic configuration integration design of hypersonic cruise aircraft with inward-turning inlets
modelling method、design method、performance improvement、aerodynamic performance、basic flow、simulation results、COONs surface、design space、method of、flow path
30
F27;TP3
the ”111” Project of China B17037
2017-09-15(万方平台首次上网日期,不代表论文的发表时间)
共14页
1349-1362