James D S;Jr Milton E V;Washington W D,Numerical investigation of aerodynamics of canardcontrolled missile using planar and grid tail fins,ADA408016,Washington D.C.,USA:NASA,2002.
[3]
Lei Juanmian;Wu Jiasheng;Meng Lingtao,Aerodynamic characteristic experimental investigation of a canard-controlled missile with a free spinning tail,Transactions of Beijing Institute of Technology,2006(01).
[4]
雷娟棉,居贤铭,吴甲生,自旋尾翼鸭式布局导弹的滚转 特性,北京理工大学学报,2004(08).
[5]
Lei Juanmian;Wu Jiasheng;Ju Xianming,Extended range guided munition aerodynamic configuration design,Journal of China Ordnance,2005(01).