[4] Liu P.Q,Duan H S, Numerical study of suction-blowing flow control technology for an airfoil, JOURNAL OF AIRCRAFT, 2010, 47(1): 229-239.
[5] Liu PQ, Wen RY, Zhang GW. Effects of canard sweep and canard-spanwise blowing magnitude on lift increment[J]. Journal of Aircraft, 2006, 43(5): 1369-1371.
[6]TIAN Yun, LIU PeiQing&FENG PeiHua. Shock control bump parametric research on supercritical airfoil [J]. Science China (Technology Science), 2011(11): 2935 -2944 , 2011.