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导弹总体计算机辅助设计研究
引用本文:汪家芸,曹剑影.导弹总体计算机辅助设计研究[J].航空学报,1994,15(8):917-920.
作者姓名:汪家芸  曹剑影
作者单位:北京航空航天大学五系
摘    要: 研究计算机辅助导弹总体设计问题。讨论导弹总体设计中气动特性模型、外形及部位安排实体造型模型、质量特性模型之间的相互联系、相互结合,提出了在总体设计阶段全面根据总体性能要求,确定设计方案的综合设计方法。所得结果能满足导弹总体设计要求,可用于分析现有导弹和设计新型导弹,也易于作进一步的扩展与更新。

关 键 词:导弹设计  计算机辅助设计  构形选  分组件  

A STUDY OF COMPUTER-AIDED MISSILE PRELIMINARY DESIGN
Wang Jiayun, Chao Jianying.A STUDY OF COMPUTER-AIDED MISSILE PRELIMINARY DESIGN[J].Acta Aeronautica et Astronautica Sinica,1994,15(8):917-920.
Authors:Wang Jiayun  Chao Jianying
Institution:5th Department,Beijing University of Aeronautics and Astronautics,Bejing,100083
Abstract:A computer-aided Missile Preliminary Design(MPD) has been studied.It contains three main models:longitudinal aerodynamic characteristics model,solid modeling model for overall configuration and subassembly layout and mass properties module. These three models are combined efficiently and the synthetic method ofdetermining design scheme can be obtained in accordance with the overall performance requirements specified in the missile preliminary de- sign phase. The results indicate that they satisfy the corresponding requirments of missile prelim- inary design. It can be used for the analysis and design for both existing and new types of missiles. It is also easy for extension,updating and spread in the foture.
Keywords:missile design  computer aided design  configuration  subassemblies
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