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非圆截面弹体气动隐身一体化设计方法

楚 亮 马东立 刘忠铁

楚 亮, 马东立, 刘忠铁等 . 非圆截面弹体气动隐身一体化设计方法[J]. 北京航空航天大学学报, 2009, 35(10): 1268-1272.
引用本文: 楚 亮, 马东立, 刘忠铁等 . 非圆截面弹体气动隐身一体化设计方法[J]. 北京航空航天大学学报, 2009, 35(10): 1268-1272.
Chu Liang, Ma Dongli, Liu Zhongtieet al. Integrated design of aerodynamic and stealthy performance for missiles with non-circular cross section[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(10): 1268-1272. (in Chinese)
Citation: Chu Liang, Ma Dongli, Liu Zhongtieet al. Integrated design of aerodynamic and stealthy performance for missiles with non-circular cross section[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(10): 1268-1272. (in Chinese)

非圆截面弹体气动隐身一体化设计方法

详细信息
    作者简介:

    楚 亮(1980-),男,陕西西安人,博士生,jjcl0623@126.com.

  • 中图分类号: V 218

Integrated design of aerodynamic and stealthy performance for missiles with non-circular cross section

  • 摘要: 从非圆截面弹体气动和隐身设计要求出发,根据多目标优化的基本概念,将Pareto方法与遗传优化搜索相结合,采用了联赛式选择复制算子、小生境技术和Pareto解集过滤器技术使解集具有较好分布特性,并在此基础上应用了旨在提高优化计算效率的响应面方法.通过采用基于N-S方程的数值求解方法计算弹体气动性能,采用物理光学法和物理绕射理论来计算其雷达散射截面积,实现了基于Pareto遗传算法的非圆截面弹体气动与隐身两个目标函数间的折衷与优化,取得了较好的优化设计结果.

     

  • [1] Mendenhall M R.战术导弹空气动力学[M].2版.洪金森译.北京:宇航出版社,1999: 6-18 Mendenhall M R.Tactical missile aerodynamics prediction methodogy [M] .2nd ed. Translated by Hong Jinsen. Beijing: Astronautically Publishing House, 1999: 6-18 (in Chinese) [2] Crossley W A, Cook A M, Fanjoy D W, et al. Using the two-branch tournament genetic algorithm for multiobjective design . AIAA-98-1914, 1998 [3] 崔逊学.多目标进化算法及其应用[M].北京:国防工业出版社,2006: 48-58 Cui Xunxue. Multiobjective evolutionary algorithms and their applications [M]. Beijing: National Defense Industry Press, 2006: 48-58 (in Chinese) [4] Myers R H, Montgomeryd C. Response surface methodology: process and product optimization using designed experiments[M]. New York: Wiley,1995:1278-1302 [5] 方开泰,马长兴.正交与均匀试验设计[M].北京:科学出版社,2001:50-59 Fang Kaitai, Ma Changxing. Research of orthogonal and uniform design[M]. Beijing: Scientific Press, 2001:50-59 (in Chinese) [6] 马东立,武哲.飞机翼面类部件的雷达散射截面计算[J].系统工程与电子技术,1994(6):33-40 Ma Dongli, Wu Zhe. The calculation of radar cross section for aircraft airfoils[J]. Journal of Systems Engineering and Electronics, 1994(6):33-40 (in Chinese) [7] 苏伟,高正红,夏露.隐身性能约束的多目标气动外形优化设计[J].空气动力学学报,2006,24(1):137-140 Su Wei, Gao Zhenghong, Xia Lu. Multiobjective optimization design of aerodynamic configuration constrained by stealth performance[J]. Acta Aerodynamica Sinica, 2006,24(1): 137-140 (in Chinese) [8] Sun J, Hansen S G. Transonic nose wave drag of axisymmetric bodies . AIAA-82-0308, 1982 [9] 何开锋,钱炜祺,刘刚,等.飞行器气动隐身一体化设计方法研究[J].空气动力学学报,2006,24(2):169-174 He Kaifeng, Qian Weiqi, Liu Gang,et al. Aircraft multi-objective design of aerodynamic and stealthy performance[J]. Acta Aerodynamica Sinica,2006,24(2):169-174(in Chinese) [10] Signal A, Lapidot E. The aerodynamic characteristic of configurations having bodies with square rectangular and circular cross sections at a Mach number of 0.75 . AIAA-87-2429,1987
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出版历程
  • 收稿日期:  2008-12-08
  • 网络出版日期:  2009-10-31

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