Volume 22 Issue 4
Apr.  2007
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HE Yun-qin, LIANG Guo-zhu. Study on solid rocket motor computer aided design/computer simulation(SRMCAD/CS) system based on dynamic combination of arithmetic components[J]. Journal of Aerospace Power, 2007, 22(4): 619-624.
Citation: HE Yun-qin, LIANG Guo-zhu. Study on solid rocket motor computer aided design/computer simulation(SRMCAD/CS) system based on dynamic combination of arithmetic components[J]. Journal of Aerospace Power, 2007, 22(4): 619-624.

Study on solid rocket motor computer aided design/computer simulation(SRMCAD/CS) system based on dynamic combination of arithmetic components

  • Received Date: 2006-06-30
  • Rev Recd Date: 2006-12-08
  • Publish Date: 2007-04-28
  • A new software model was developed to obtain the desired design/simulation arithmetic by combining arithmetic components dynamically according to rocket motor designers’ design/simulation tasks.This software model could be used to finish a variety of SRMCAD/CS tasks while offering excellent expandability for software system.The purpose of this research is to create a standard and open arithmetic component interface system,whereby a reusable,expandable arithmetic components library and a combined arithmetic components mechanism could be established.In this way,the designers’ tasks of compiling design/simulation arithmetic can be turned to combine dynamically into a desired one using the existing arithmetic components.This software model enables the designers to reuse the existing arithmetic in the arithmetic component library,while maintaining the liberty of designers for easier and efficient work.

     

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  • [1]
    Roys G P.User's manual for solid propulsion optimization code[R].AD-A 108224,1981.
    [2]
    Jacgues L,Legagneux D.Computer aided preliminary design of ARIANE 5 SRM[R].AIAA 87-1738.
    [3]
    Dick W A,Heath M T,Fiedler R A.Integrated 3-D simulation of solid propellant rockets[R].AIAA 2001-3949.
    [4]
    Alavilli P V S,Tafti D,Najjar F.The development of an advanced solid-rocket flow simulation program ROCFLO[R].AIAA 2000-0824.
    [5]
    梁国柱,张卫华,郭红杰,等.固体火箭发动机集成方案设计系统SRMCAD[J].固体火箭技术,2003,26(3):18-21.LIANG Guozhu,ZHANG Weihua,GUO Hongjie,et al.Brief introduction of solid rocket motor integrated conceptual design system SRMCAD[J].Journal of Solid Rocket Technology,2003,26(3):18-21.
    [6]
    张延伟,梁国柱,张卫华.基于Pro/Engineer的固体火箭发动机装药CAD系统实现[A].固体火箭推进技术学术会议论文集(发动机分册)[C].上海:中国宇航学会固体火箭推进专业委员会第二十一届年会,2004.
    [7]
    鲍福廷,郭大庆,赵飞,等.固体火箭发动机喷管集成设计分析技术研究[A].固体火箭推进技术学术会议论文集(发动机分册)[C].上海:中国宇航学会固体火箭推进专业委员会第二十一届年会,2004.
    [8]
    王建儒,刘霓生,陈林泉.固体火箭发动机喷管热结构CAD[A].固体火箭推进技术学术会议论文集(发动机分册)[C].湖南张家界:中国宇航学会固体火箭推进专业委员第二十届年会,2003.
    [9]
    徐伟,梁国柱.固体火箭发动机喷管应变应力场计算与软件开发[A].中国宇航学会2005年固体火箭推进第22届年会论文集(发动机分册)[C].四川成都:2005.
    [10]
    鲍福廷,蔡体敏.固体火箭发动机集成初步设计CAD系统研究[J].西北工业大学学报,2001,19(4):498-501.BAO Futing,CAI Timin.Some progress in development of Chinese in tegrated preliminary CAD design of solid rocket motors[J].Journal of Northwestern Polytechnical University,2001,19(4):498-501.
    [11]
    鲍福廷,李逢春.固体发动机装药CAD[J].固体火箭技术,1994,(3):1-7.BAO Futing,LI Fengchun.Computer aided design of propellant grains for solid rocket motors[J].Journal of Solid Rocket Technology,1994,(3):1-7.
    [12]
    Brooks F.人月神话[M].北京:清华大学出版社,2003.
    [13]
    Larman C.Applying UML and Patterns[M].北京:中国电力出版社,2005.
    [14]
    Chappell D.Understanding.Net[M].武汉:华中科技大学出版社,2004.
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