Citation: | LEI Juan-mian, WU Jia-sheng, MENG Ling-tao. Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail[J].JOURNAL OF BEIJING INSTITUTE OF TECHNOLOGY, 2006, 15(1): 36-38. |
[1] |
Auman L M. Aerodynamic characterist ics of a canar dcontrolled missile with a freespinning tail[R]. AIAA 98-0410, 1998.
|
[2] |
Qi Zaikang. Guided ammunition technolog y [M]. Beijing; Beijing I nst itute of T echnolog y Press, 2002. (inChinese)
|
[3] |
Lei Juanmian, Ju Xianming, Wu Jiasheng. Rolling character istics of canardcontrolled missiles with a freespinning tail[J]. Tr ansact ions of Beijing Institute of Technology , 2004, 24(8); 657-659. (in Chinese)
|
[4] |
Wu Jiasheng , Lei Juanmian. Trends in the developmentof aerody namic configur ation of guided w eapons and relevant aerodynamic techniques[J]. Transactions of BeijingInstitute of Technology, 2003, 23(6); 665 -670. (inChinese)
|
[5] |
L Guoxin. Winged missiles aerodynamic design [M]. Beijing: Astronautic Press, 1991. (in Chinese)
|
[6] |
Yu Benshui. Antiaircraft missile overall design [M]. Beijing: Astronautic Press, 1995. (in Chinese)
|