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支柱式沉浸水橇降载性能相关影响因素

高霄鹏 孙培成 董祖舜 吴彬 魏可可

高霄鹏, 孙培成, 董祖舜, 等 . 支柱式沉浸水橇降载性能相关影响因素[J]. 北京航空航天大学学报, 2016, 42(2): 236-242. doi: 10.13700/j.bh.1001-5965.2015.0079
引用本文: 高霄鹏, 孙培成, 董祖舜, 等 . 支柱式沉浸水橇降载性能相关影响因素[J]. 北京航空航天大学学报, 2016, 42(2): 236-242. doi: 10.13700/j.bh.1001-5965.2015.0079
GAO Xiaopeng, SUN Peicheng, DONG Zushun, et al. Influence of hydro-ski load reducing performance corresponding on some parameters[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(2): 236-242. doi: 10.13700/j.bh.1001-5965.2015.0079(in Chinese)
Citation: GAO Xiaopeng, SUN Peicheng, DONG Zushun, et al. Influence of hydro-ski load reducing performance corresponding on some parameters[J]. Journal of Beijing University of Aeronautics and Astronautics, 2016, 42(2): 236-242. doi: 10.13700/j.bh.1001-5965.2015.0079(in Chinese)

支柱式沉浸水橇降载性能相关影响因素

doi: 10.13700/j.bh.1001-5965.2015.0079
基金项目: 航空科学基金(20132316001)
详细信息
    作者简介:

    高霄鹏 女,博士,副教授。主要研究方向:船舶性能流体力学。 E-mail:18627093611@163.com;孙培成 男,硕士研究生。主要研究方向:船舶性能流体力学。Tel.:15327236784 E-mail:1229726215@qq.com

    通讯作者:

    孙培成,Tel.:15327236784 E-mail:1229726215@qq.com

  • 中图分类号: V221+.3

Influence of hydro-ski load reducing performance corresponding on some parameters

  • 摘要: 支柱式沉浸水橇可降低水陆两栖飞机着水运动中的冲击载荷,其降载效果与水陆两栖飞机的运动参数有关。利用一般耦合算法对水陆两栖飞机着水运动进行仿真,并将结果与相关试验值比对以验证仿真方法的有效性。采用此方法研究了水橇着水角、飞机着水水平速度与飞机着水垂向速度对支柱式沉浸水橇降载性能的影响。结果表明:水橇着水角、飞机着水水平速度与飞机着水垂向速度对水橇降载性能影响显著,合理地控制水橇的着水角与速度,可获得良好的降载效果。

     

  • [1] FISHER L J.Model ditching investigation of three airplanes equipped with hydro-skis[R].[S.l.:s.n.],1950.
    [2] WADLIN K L,MCGEHEE J R.Planning characteristics of six surfaces representative of hydro-ski forms[R].[S.l.:s.n.],1950.
    [3] PETYNIA W W,HASSON D F,SPOONER S H.Aerodynamic and hydrodynamic characteristics of a proposed supersonic multijet water-baesed hydro-ski aircraft with a variable-incidence wing[R].[S.l.:s.n.],1957.
    [4] WADLIN K L,RAMSEN J A.Tank investigation of the Grumman JRF-5 airplane fitted with hydro-skis suitable for operation on water,snow,and ice[R].[S.l.:s.n.],1950.
    [5] RAMSEN J A,GRAY G R.Tank investigation of the Grumman JRF-5 airplane with a single hydro-ski and an extended afterbody[R].[S.l.:s.n.],1951.
    [6] COFFEE JR C W.Tank tests of 1/8-size powered dynamic of the Martin PBM-5 seaplane equipped with a single EDO hydro-ski[R].[S.l.:s.n.],1955.
    [7] VAUGHAN JR V L.The hydrodynamic characteristic of submerged lifting surface having a shape suitable for hydro-ski application[R].[S.l.:s.n.],1959.
    [8] MELIS M E.Finite element simulation of a space shuttle solid rocket booster aft skirt splashdown using an arbitrary lagrangian-eulerian approach[R].[S.l.:s.n.],2003.
    [9] 贺谦,李元生,李磊,等.基于ALE方法的飞机水面降落过程[J].爆炸与冲击,2010,30(2):125-130. HE Q,LI Y S,LI L,et al.On dynamic structral response on an airplane landing onto water[J].Explosion and Shock Waves,2010,30(2):125-130(in Chinese).
    [10] 刘静.地效飞机入水载荷数值分析[D].南京:南京理工大学,2011:61. LIU J.Numerical analysis about high-speed entry water of wing-in-ground-effect-plane[D].Nanjing:Nanjing University of Science and Technology,2011:61(in Chinese).
    [11] 刘翔.飞机水上迫降的运动特性分析和讨论[D].武汉:武汉理工大学,2012:47. LIU X.Analysis and discussion on hydrodynamic characteristics of aircraft during ditching[D].Wuhan:Wuhan University of Technology,2012:47(in Chinese).
    [12] 罗琳胤,杨仕福,吕继航.水陆两栖飞机着水响应模型与数值分析[J].机械设计,2013,30(8):86-89. LUO L Y,YANG S F,LYU J H.Analysis and numerical simulation of water landing response model for amphibian[J].Journal of Machine Desigin,2013,30(8):86-89(in Chinese).
    [13] 张韬,李书,江翔,等.民用飞机水上迫降分析模型和数值仿真[J].南京航空航天大学学报,2010,42(3):392-394. ZHANG T,LI S,JIANG X,et al.Analysis model and numerical simulation for civil plane ditching[J].Journal of Nanjing University of Aeronautics and Astronautics,2010,42(3):392-394(in Chinese).
    [14] 魏照宇,石秀华,王银涛,等.水下航行器高速斜入水冲击的探索仿真研究[J].西北工业大学学报,2010,28(5):718-723. WEI Z Y,SHI X H,WANG Y T,et al.Explotion high-speed oblique water entry impact of an underwater vehicle[J].Journal of Northwestern Polytechnical University,2010,28(5):718-723(in Chinese).
    [15] 闫明.基于有限体积法的飞机水上迫降[D].武汉:武汉理工大学,2012:54. YAN M.Numerical investigation on aircraft ditching's characteristic of motion by FVM[D].Wuhan:Wuhan University of Technology,2012:54(in Chinese).
    [16] 郭保东,屈秋林,刘沛清,等.混合翼身布局客机SAX-40水上迫降力学性能数值研究[J].航空学报,2013,34(11):2443-2451. GUO B D,QU Q L,LIU P Q,et al.Ditching performance of silent aircraft SAX-40 in hybrid wing-body configuration[J].Acta Aeronautica et Astronautica Sinica,2013,34(11):2443-2451(in Chinese).
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出版历程
  • 收稿日期:  2015-02-05
  • 网络出版日期:  2016-02-20

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