Volume 42 Issue 2
Feb.  2016
Turn off MathJax
Article Contents
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)

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

doi: 10.13700/j.bh.1001-5965.2015.0079
  • Received Date: 05 Feb 2015
  • Publish Date: 20 Feb 2016
  • The impact load of amphibious aircraft could be reduced efficiently by use of hydro-ski, and the load reducing effect of hydro-ski is obviously relevant with some motion parameters of the aircraft. General coupling method was used to simulate the water landing performance of an amphibious aircraft and the comparison between the calculated results and the model test ones was carried out to prove the effectiveness of the simulation method. The study analyzed the influence of hydro-ski touch attitude angle,aircraft touch horizontal velocity and vertical velocity on load reducing performance of the hydro-ski. Conclusion could be obtained that the influence of the above three factors on hydro-ski load reducing performance is relatively remarkable, and the impact load could be reduced more efficiently with the proper hydro-ski attitude angle and velocities.

     

  • loading
  • [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).
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(952) PDF downloads(465) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return