Citation: | DONG Jingang, JIN Jialin, LI Guangliang, QIN Yongming, MA Handong. Research on test technology of dynamic force measurement of rotating missile in wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2020, 34(4): 81-86. DOI: 10.11729/syltlx20190119 |
[1] |
王波兰, 李克勇, 杨永强.近程/末端防御旋转导弹发展及关键技术综述[J].上海航天, 2017, 34(s1):1-6. http://www.cnki.com.cn/Article/CJFDTotal-SHHT2017S1001.htm
WANG B L, LI K Y, YANG Y Q. Review of development and key techniques of rolling airframe missiles[J]. Aerospace Shanghai, 2017, 34(s1):1-6. http://www.cnki.com.cn/Article/CJFDTotal-SHHT2017S1001.htm
|
[2] |
李惠芝, 成楚之.旋转导弹的气动布局[J].战术导弹技术, 1989(3):4-10. http://www.cnki.com.cn/Article/CJFDTotal-ZSDD198903002.htm
LI H Z, CHENG C Z. Aerodynamic layout of a rotating missile[J]. Tactical missile technology, 1989(3):4-10. http://www.cnki.com.cn/Article/CJFDTotal-ZSDD198903002.htm
|
[3] |
杨安生.便携式红外寻的防空导弹——气动外形[J].上海航天, 1998(2):52-57. http://www.cnki.com.cn/Article/CJFDTotal-SHHT802.010.htm
YANG A S. Portable infrared homing air-defense missile——aerodynamic configuration[J]. Aerospace Shanghai, 1998(2):52-57. http://www.cnki.com.cn/Article/CJFDTotal-SHHT802.010.htm
|
[4] |
张宏俊, 吴强, 张铁兵.舰载末端防御导弹及其技术发展[J].上海航天, 2013, 30(5):1-6. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=shht201305001
ZHANG H J, WU Q, ZHANG T B. Technology and development of ship-based terminal defense missile[J]. Aerospace Shanghai, 2013, 30(5):1-6. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=shht201305001
|
[5] |
张平峰, 周志超.鸭式布局旋转导弹气动特性研究[J].上海航天, 2013, 30(3):45-49. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=shht201303010
ZHANG P F, ZHOU Z C. Research on aerodynamics of canard rolling airframe missile[J]. Aerospace Shanghai, 2013, 30(3):45-49. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=shht201303010
|
[6] |
WALTER R F. Free gyro imaging IR sensor in Rolling Airframe Missile application[R]. Raython Missile Systems, 1999.
|
[7] |
任天荣, 马建敏.拉姆导弹总体构型设计分析[J].弹箭与制导学报, 2013, 33(3):25-32. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=djyzdxb201303007
REN T R, MA J M. Analysis on preliminary layout design of RAM missile[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2013, 33(3):25-32. http://www.wanfangdata.com.cn/details/detail.do?_type=perio&id=djyzdxb201303007
|
[8] |
叶尧卿.便携式红外寻的防空弹道设计[M].北京:中国宇航出版社, 2006. http://www.cnki.com.cn/article/cjfdtotal-shht805.010.htm
YE Y Q. Portable infrared homing air defense trajectory design[M]. Beijing:China Astronautic Publishing House, 2006. http://www.cnki.com.cn/article/cjfdtotal-shht805.010.htm
|
[9] |
余奇华, 敬代勇.旋转尾翼鸭式布局导弹数值模拟[J].战术导弹技术, 2012(2):16-19. http://www.cqvip.com/QK/93603X/201202/41553090.html
YU Q H, JING D Y. Numerical simulation of a canard missile with a spinning tail fin[J]. Tactical Missile Technology, 2012(2):16-19. http://www.cqvip.com/QK/93603X/201202/41553090.html
|
[10] |
雷娟棉, 吴甲生, 郑志伟.弹箭旋转空气动力效应研究进展[C]//第十四届全国分离流、流动控制会议论文集. 2013.
LEI J M, WU J S, ZHENG Z W. Research progress of spinning aerodynamic effects of rockets[C]//Proceedings of the 14th National Conference on Separation, Vortex and Flow Control. 2013.
|
[11] |
SEGINER A. Magnus effects on spinning transonic missiles[R]. AIAA-83-2146, 1983.
|
[12] |
SEGINER A. Magnus effects at high angles of attack and critical Reynolds numbers[R]. AIAA-83-2145, 1983.
|
[13] |
SEGINER A, ROSENWASSER I. Magnus effects on spinning transonic finned missiles[J]. Journal of Spacecraft and Rockets, 1986, 23(1):31-38. DOI: 10.2514/3.25080
|
[14] |
NYGAARD T A, MEAKIN R L. Aerodynamic analysis of a spinning missile with dithering canards[J]. Journal of Spacecraft and Rockets, 2004, 41(5):726-734. DOI: 10.2514/1.13075
|
[15] |
BURKHALTER J E, HEISER M A. Linear aerodynamic analysis of a spinning missile with dithering canards[R]. AIAA-2002-2800, 2002.
|
[16] |
SHENG C H, WANG X. Aerodynamic analysis of a spinning missile with dithering canards using a high order unstructured grid scheme[R]. AIAA-2009-1090, 2009.
|
[17] |
BLADESE L, MARCUM D L, MITCHELL B. Simulation of spinning missile flow fields using U2NCLE[R]. AIAA-2002-2797, 2002.
|
[18] |
HALL L H. Rolling airframe missile aerodynamic predictions using a chimera approach for dithering canards[R]. AIAA-2002-0405, 2002.
|
[19] |
TISSERAND L E. Aerodynamics of a rolling airframe missile[R]. ADA111769, 1982.
|
[20] |
GOLD R, BUSAN R. Design and implementation of a full-scale spinning missile model with active canard control[R]. AIAA-94-0721, 1994.
|
[21] |
DILLEY A D, MCBRIDE R T, YUKI V A, et al. Dynamic wind tunnel test of an innovative rolling missile model[R]. AIAA-2008-4032, 2008.
|
[22] |
吴甲生, 徐文熙. BS-7基本旋转模型magnus风洞试验(一)[J].兵工学报弹箭分册, 1987(4):15-21. http://www.cnki.com.cn/Article/CJFDTotal-DJZD198704002.htm
|
[23] |
吴甲生, 徐文熙, 居贤铭.低阻增程弹风洞试验研究[J].北京理工大学学报, 1989(2):29-34. http://www.ixueshu.com/document/4eb12ee3a8f9232ffd84b0cc68808f88318947a18e7f9386.html
WU J S, XU W X, JU X M.Wind tunnel experimental investigation of low extended range projectiles[J]. Transactions of Beijing Institute of Technology, 1989(2):29-34. http://www.ixueshu.com/document/4eb12ee3a8f9232ffd84b0cc68808f88318947a18e7f9386.html
|
[24] |
吴甲生, 徐文熙.旋转弧翼身组合体空气动力特性实验研究[J].气动实验与测量控制, 1988, 2(1):41-50. http://www.cnki.com.cn/Article/CJFDTotal-LTLC198801005.htm
|