Numerical investigation of aerodynamic flow actuation produced by surface plasma actuator on 2D oscillating airfoil
pressure force、dynamic stall、flow control、glow discharge plasma、pressure fluctuation、reduced frequency、power consumption、lift coefficient、angle of attack、turbulent flow、dynamic change、control scheme
29
V21;O4
This research was supported by the Basic Science Research Program through the National Research Foundation of Korea NRF funded by the Ministry of Science, ICT&Future Plan-ning2013R1A1A1012693;was conducted at High-Speed Vehicle Research Center of KAIST with the support of Defense Acquisition Program Administration;Agency for Defense Development
2016-09-02(万方平台首次上网日期,不代表论文的发表时间)
共11页
882-892