Turbulent boundary layer separation control using plasma actuator at Reynolds number 2000000
high Reynolds number、separation control、boundary layer separation、turbulent boundary layer、lift coefficient、particle image velocimetry、experimental investigation、wind tunnel、strain gauge balance、experimental study、angle of attack、laser Doppler、test model、method of
29
O35;TV1
the Exploration Foundation of Weapon Systems 7130711
2016-11-10(万方平台首次上网日期,不代表论文的发表时间)
共10页
1237-1246