留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

飞翼布局气动方案优选和试验验证

鲍君波 王钢林 武哲

鲍君波, 王钢林, 武哲等 . 飞翼布局气动方案优选和试验验证[J]. 北京航空航天大学学报, 2012, (2): 180-184.
引用本文: 鲍君波, 王钢林, 武哲等 . 飞翼布局气动方案优选和试验验证[J]. 北京航空航天大学学报, 2012, (2): 180-184.
Bao Junbo, Wang Ganglin, Wu Zheet al. Optimization and experimental verification for aerodynamic scheme of flying-wing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 180-184. (in Chinese)
Citation: Bao Junbo, Wang Ganglin, Wu Zheet al. Optimization and experimental verification for aerodynamic scheme of flying-wing[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012, (2): 180-184. (in Chinese)

飞翼布局气动方案优选和试验验证

详细信息
  • 中图分类号: V 221

Optimization and experimental verification for aerodynamic scheme of flying-wing

  • 摘要: 提出综合考虑飞翼布局隐身性能和气动性能的平面形状特征参数,分析了方案优选中的约束关系.采用参数化方法构建了三维曲面模型,并将物面网格划分流程进行自动化封装,通过更改设计参数准确快速地得到新方案的物面网格.应用基于Euler方程的数值方法进行布局方案的气动性能计算分析,在重点方案的分析中加入黏性修正;应用高频近似方法估算方案的隐身性能.以巡航状态作为设计点,在隐身性能的约束下,应用分析-修正的方法完成了气动布局方案优选,并对最终选定的方案进行风洞试验验证,证明该方案有进一步研究的价值.

     

  • [1] 刘玉仁,陈明璟,张甲林.无人机的发展分析[J].舰船电子工程,2008,28(6):63-66 Liu Yuren,Chen Mingjing,Zhang Jialin.Analysis of the development of UAV [J].Ship Electronic Engineering,2008,28(6):63-66(in Chinese)
    [2] 刘重阳.国外无人机技术的发展[J].舰船电子工程,2010,30(1):19-23 Liu Chongyang.Development of UAV technology abroad[J].Ship Electronic Engineering,2010,30(1):19-23(in Chinese)
    [3] 詹光,孙颖,蔡为民.新型航空武器装备——无人作战飞机[J].飞机设计,2009,29(4):75-80 Zhan Guang,Sun Ying,Cai Weimin.Unmanned combat air vehicle—a new style air weapon platform [J].Aircraft Design,2009,29(4):75-80(in Chinese)
    [4] 魏金钟,王光耀,顾诵芬.无人作战飞机对地攻击费效比分析[J].北京航空航天大学学报,2009,35(6):709-713 Wei Jinzhong,Wang Guangyao,Gu Songfen.Cost efficiency analysis of attack UCAV [J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(6):709-713(in Chinese)
    [5] Wood R M,Bauer S X S.Flying wings/flying fuselage .AIAA-2001-0311,2001
    [6] Grellmann H W.B-2 Aerodynamic Design .AIAA-90-1802,1990
    [7] 张洋,高纪朝,周昊,等.X-47B——美国海军舰载无人战斗机[J].飞航导弹,2009(1):12-14 Zhang Yang,Gao Jichao,Zhou Hao,et al.X-47B—US Navy carrier based unmanned combat aircraft [J].Winged Missiles Journal,2009(1):12-14(in Chinese)
    [8] 阿雯,车易.波音公司披露X-45C改进型——幻影雷无人战斗机[J].飞航导弹,2009(11):1-2 A Wen,Che Yi.Boeing X-45C improved disclosure—Phantom Thunder UCAV [J].Winged Missiles Journal,2009(11):1-2(in Chinese)
    [9] 关军,魏国福.欧洲六国联合研制神经元无人战斗机[J].飞航导弹,2006(7):17-19 Guan Jun,Wei Guofu.Six European countries unmanned combat aircraft jointly developed neurons [J].Winged Missiles Journal,2006(7):17-19(in Chinese)
    [10] Nangia R K,Palmer M E.A comparative study of UCAV type wing planforms-aero performance and stability considerations .AIAA-2005-5078,2005
    [11] 李天,武哲,李敬.飞机外形参数的气动与隐身综合优化设计[J].北京航空航天大学学报,2001,27(1):76-78 Li Tian,Wu Zhe,Li Jing.Integrated aerodynamic stealth optimal design of aircraft configuration parameters [J].Journal of Beijing University of Aeronautics and Astronautics,2001,27(1):76-78(in Chinese)
    [12] 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].空气动力学报,2006,24(1):137-140 Su Wei,Gao Zhenghong,Xia Lu.Multiobjective optimization design of aerodynamic configuration constrained by stealth performance [J].Acta Aerodynmica Sinica,2006,24(1):137-140(in Chinese)
    [13] 王钢林,刘虎,武哲,等.一种Cartesian气动网格的自适应划分算法[J].应用力学学报,2008,25(2):274-278 Wang Ganglin,Liu Hu,Wu Zhe,et al.Adaptive mesh algorithm for generating Cartesian aerodynamic grids [J].Chinese Journal of Applied Mechanics,2008,25(2):274-278(in Chinese)
    [14] 施敬,杨波,周小勇.从UG数模到MGAERO网格的转换[J].洪都科技,2004(3):26-32 Shi Jing,Yang Bo,Zhou Xiaoyong.Transformation from UG mathematical model to MGAERO grid [J].Hongdu Science and Technology,2004(3):26-32(in Chinese)
    [15] Tom R B,Alfred G S.Optimization of aircraft configuration for minimum drag .AIAA-2010-3000,2010
    [16] 张考,马东立.军用飞机生存力与隐身设计[M].北京:国防工业出版社,2006:120-138 Zhang Kao,Ma Dongli.Military aircraft survivability and stealth design [M].Bejing:National Defence Industrial Press,2006:120-138(in Chinese)
    [17] 范洁川.风洞试验手册[M].北京:航空工业出版社,2002:1-722 Fan Jiechuan.Wind tunnel test manual [M].Beijing:Aviation Industrial Press,2002:1-722(in Chinese)
  • 加载中
计量
  • 文章访问数:  2769
  • HTML全文浏览量:  132
  • PDF下载量:  732
  • 被引次数: 0
出版历程
  • 收稿日期:  2011-03-17
  • 网络出版日期:  2012-02-29

目录

    /

    返回文章
    返回
    常见问答