Numerical evaluation of passive control of shock wave/boundary layer interaction on NACA0012 airfoil using jagged wall
shock waves、aerodynamic characteristics、rectangular shape、numerical studies、numerical results、triangular shape、numerical method、drag coefficient、shock structure、flow separation、empirical study、boundary layers、angle of attack、transonic flow、flow field
32
TK1;O35
2016-11-07(万方平台首次上网日期,不代表论文的发表时间)
共13页
792-804