In order to solve the problem of long design period, low design efficiency and high investment cost in the traditional design process of rockets, the rocket digital design system was built. The system integrated some key technologies, such as a variety of CAD/CAE software, the design process of application parameterization, three dimensional parameterized automatic modeling of missile body and optimization design of overall structural parameters, which achieved the design, optimization, simulation and other digital processes of rocket products. The feasibility of the system in the design of different types of rockets was verified by the design of key technologies. This system not only greatly improves the design efficiency of rocket, but also provides a theoretical reference for the digital design of other conventional ammunition.
ZHANG Xiaodong
,
CAO Hongsong
,
YUAN Yuwen
,
GUO Xiangxiang
,
SONG Xuhui
. Research on Digital Design of Rocket[J]. Journal of Projectiles, Rockets, Missiles and Guidance, 2017
, 37(6)
: 40
-44
.
DOI: 10.15892/j.cnki.djzdxb.2017.06.009
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[1] 佚名. PRODAS-基于工程算法的火箭弹、导弹、炮弹快速设计平台[EB/OL].[2017-03-04].http//www. sinosofts.com.cn/col.jsp?id=113.
[2] 史毛毛, 曹红松, 李士利, 等. 石油射孔弹数字化设计软件开发[J].测井技术, 2015, 39(1): 167-173.
[3] 史慕溪. 弹箭战斗部数字化设计系统开发[D].太原: 中北大学, 2015: 2-3.
[4] 孙厚朝. 基于UG的数字化设计技术研究[D].太原: 中北大学, 2003: 9-32.
[5] 梅小宁, 杨树兴. 基于UG二次开发的参数化建模方法在优化设计中的应用[J].科技导报, 2010, 28(3): 29-30.
[6] 肖飞, 张为华, 解红雨, 等. 火箭弹数字化设计平台研究与设计[C]//中国航空学会航空动力学分会火箭发动机专业委员会. 火箭推进技术学术会议文集. 长沙: 国防科技大学出版社, 2006: 203-206.
[7] 周长省, 鞠玉涛, 朱福亚,等. 火箭弹设计理论[M].北京: 北京理工大学出版社, 2014: 71-253.
[8] 沈仲书, 刘亚飞. 弹丸空气动力学[M].北京: 国防工业出版社, 1984: 284-384.
[9] 明日科技. Visual C++从入门到精通[M].3版. 北京: 清华大学出版社, 2012: 480-500.