SolidWorks某型导弹总体结构设计与气动参数分析

摘要本文某型号地空导弹为例，查阅相关资料，结合实际，梳理相关数据及文字，进行整理，建立了适用于地空导弹总体快速设计的气动三文模型,其中动力系统采用整体式固体火箭冲压发动机。本研究主要集中在以下几个方面：
    1、参照该型号导弹，依照标准与经验，设定相应地导弹参数；
    2、根据设定的导弹数据，使用SolidWorks软件对其进行三文建模；
    3、基于三文模型，根据导弹工作条件，利用Datcom软件对改变后的导弹的气动力参数进行预估。25477
关键词：   导弹总体结构设计   三文建模气动力预估地空导弹
毕业论文设计说明书外文摘要
Title The certain type of missile general structure design and analysis of aerodynamic parameters
Abstract
Developed in this paper， the former Soviet union "Sam - 2" missile as an example， with reference to the northwestern polytechnical university courses - missile overall structure design， design specifications， combing the related data and text of articles， in order to set up suitable for surface to air missile overall 3 d model of rapid design of pneumatic， including power system adopts the integral solid rocket ramjet.
     This research mainly concentrated in the following aspects：
     1. Improved the exquisite course of northwestern polytechnical university - missile overall structure design， design specification of aerodynamic shape model， and the related data and information for validation， and indicate the source；
2. According to relevant data， using SolidWorks software for 3 d modeling， 3 d model is established. And according to the model， the fast accurate missile aerodynamic performance parameters are given；
3. At last， using software Datcom to estimate the aerodynamic force of accuracy， input basic parameters based on the three-dimensional model， according to the corresponding program， the output of aerodynamic parameters， and report to and get the corresponding results.
Analysis causes of the error， pointed out the direction for future development. The development of our country has important reference value for surface to air missile.
Keywords：Missile overall structure design      3D modeling    Aerodynamic forecast   surface-to-air missile
目    次
1 绪论    1
1.1 本文的研究目的及意义    1
1.2   地空导弹发展综述及趋势    1
1.3 国内外研究发展现状    2
1.4 主要研究内容    3
2 总体设计    4
2.1 概述    4
2.2弹道设计与过载计算    4
2.3 质量分配    5
2.3.1 I级与II级质量分配    5
2.2.2 质量分布假设    6
2.4 舱段划分    6
2.4.1 坐标系建立：    6
2.4.2 舱段划分    6
2.5 气动外形设计    7
2.5.1 翼面设计    7
2.4.2 弹身设计    21
3 导弹总体外形结构    23
3.1绪论    23
3.2 绘图    23
3.3说明    24
4 Datcom气动参数分析    26
4.1 Datcom软件功能及使用    26
4.2 Datcom气动参数分析    27
4.3Datcom计算结果与总体设计计算结果的比较    28
结论    30
致谢    31 SolidWorks某型导弹总体结构设计与气动参数分析:http://www.751com.cn/jixie/lunwen_19297.html