Volume 35 Issue 5
Nov.  2021
Turn off MathJax
Article Contents
GAO L H,HUANG L T,FU H,et al. Wind tunnel test for aerodynamics of wing-in-ground craft flying near smooth/wavy surface[J]. Journal of Experiments in Fluid Mechanics, 2021,35(5):68-74. doi: 10.11729/syltlx20200077
Citation: GAO L H,HUANG L T,FU H,et al. Wind tunnel test for aerodynamics of wing-in-ground craft flying near smooth/wavy surface[J]. Journal of Experiments in Fluid Mechanics, 2021,35(5):68-74. doi: 10.11729/syltlx20200077

Wind tunnel test for aerodynamics of wing-in-ground craft flying near smooth/wavy surface

doi: 10.11729/syltlx20200077
  • Received Date: 2020-06-19
  • Rev Recd Date: 2020-07-18
  • Available Online: 2021-09-29
  • Publish Date: 2021-11-05
  • In order to investigate the aerodynamics of the wing-in-ground craft flying near wavy surface the dedicated wavy ground floor and moving wavy belt are devised to simulate the real water wave with the height of one meter. The wavy ground floor is capable of varying its vertical and horizontal position. The moving wavy belt which contains two waves on the belt is suitable for the wind tunnel test of the wing-in-ground craft flying over all the phases of the wave. The wind tunnel test has been carried out which simulates the wing-in-ground craft flying in the sky, near smooth surface and wavy surface by means of flat ground floor, wavy ground floor and moving wavy belt, respectively. The wind tunnel test results show that propellers and the floor have a coupling effect on the taking-off and landing aerodynamics of the wing-in-ground craft, instead of simple superposition. What is more, the aerodynamic loads of the wing-in-ground craft fluctuate dramatically over the various phases of the wave.
  • loading
  • [1]
    李先达. 实用地效飞行器技术发展述评[J]. 前沿科学,2011,5(3):22-31. doi: 10.3969/j.issn.1673-8128.2011.03.005

    LI X D. Review on key technologies to develop practical WIG craft[J]. Frontier Science,2011,5(3):22-31. doi: 10.3969/j.issn.1673-8128.2011.03.005
    [2]
    屈秋林,刘沛清,秦绪国. 地效飞行器波浪地面飞行气动性能数值研究[J]. 航空学报,2007,28(6):1327-1333. doi: 10.3321/j.issn:1000-6893.2007.06.009

    QU Q L,LIU P Q,QIN X G. Numerical research on aerodynamic characteristics of WIG craft flying over wavy ground[J]. Acta Aeronautica et Astronautica Sinica,2007,28(6):1327-1333. doi: 10.3321/j.issn:1000-6893.2007.06.009
    [3]
    乐挺,王立新. 地效飞机的纵向稳定性和气动布局特点研究[J]. 飞行力学,2007,25(3):5-8. doi: 10.3969/j.issn.1002-0853.2007.03.002

    YUE T,WANG L X. A study on longitudinal stability and configu-ration characteristics of wing-in-ground effect craft[J]. Flight Dyna-mics,2007,25(3):5-8. doi: 10.3969/j.issn.1002-0853.2007.03.002
    [4]
    秦绪国,刘沛清,屈秋林. 翼型波浪水面巡航地面效应数值模拟[J]. 北京航空航天大学学报,2011,37(3):295-299, 304. doi: 10.13700/j.bh.1001-5965.2011.03.001

    QIN X G,LIU P Q,QU Q L. Numerical simulation on aerodynamics of airfoil flying over wavy water surface[J]. Journal of Beijing University of Aeronautics and Astronautics,2011,37(3):295-299, 304. doi: 10.13700/j.bh.1001-5965.2011.03.001
    [5]
    邢福,吴宝山,朱仁庆. 地效翼气动力特性的数值预报[J]. 船舶力学,2004,8(6):19-30. doi: 10.3969/j.issn.1007-7294.2004.06.003

    XING F,WU B S,ZHU R Q. Investigation on numerical prediction of WIG’s aerodynamics[J]. Journal of Ship Mechanics,2004,8(6):19-30. doi: 10.3969/j.issn.1007-7294.2004.06.003
    [6]
    顾璇. 近地/海运动过程中的空气动力学分析[D]. 哈尔滨: 哈尔滨工程大学, 2009.

    GU X. Aerodynamic analysis on near-ground/sea motion[D]. Harbin: Harbin Engineering University, 2009.
    [7]
    杨美,杨韡,杨志刚. 地效翼地面粘性效应风洞试验研究[J]. 空气动力学学报,2015,33(1):82-86. doi: 10.7638/kqdlxxb-2013.0002

    YANG M,YANG W,YANG Z G. Wind tunnel test of ground viscous effect on wing aerodynamics[J]. Acta Aerodynamica Sinica,2015,33(1):82-86. doi: 10.7638/kqdlxxb-2013.0002
    [8]
    周丹杰,曹德一,东海宁. 国内外地效飞行器实验研究[J]. 战术导弹技术,2010(3):32-36. doi: 10.16358/j.issn.1009-1300.2010.03.002

    ZHOU D J,CAO D Y,DONG H N. Experimental research on Wing-in-ground-effect vehicle[J]. Tactical Missile Technology,2010(3):32-36. doi: 10.16358/j.issn.1009-1300.2010.03.002
    [9]
    HIEMCKE C. NACA 5312 in ground effect: Wind tunnel and panel code studies[R]. AIAA-97-2320, 1997. doi: 10.2514/6.1997-2320
    [10]
    陈新, 单雪雄. 三维机翼掠海飞行时非定常气动力和兴波的数值计算[C]//2003空气动力学前沿研究研讨会论文集. 北京: 中国宇航出版社, 2003: 132-137.
    [11]
    杨炯,梁鉴,李征初. 活动地板关键技术研究[J]. 实验流体力学,2008,22(4):68-71. doi: 10.3969/j.issn.1672-9897.2008.04.015

    YANG J,LIANG J,LI Z C. Key technical research on developing moving belt ground proximity[J]. Journal of Experiments in Fluid Mechanics,2008,22(4):68-71. doi: 10.3969/j.issn.1672-9897.2008.04.015
    [12]
    李征初,杨炯,梁鉴,等. Φ3.2 m风洞活动地板系统研制[J]. 实验流体力学,2011,25(4):89-93. doi: 10.3969/j.issn.1672-9897.2011.04.017

    LI Z C,YANG J,LIANG J,et al. Development of moving belt floor in Φ3.2 m wind tunnel[J]. Journal of Experiments in Fluid Mech-anics,2011,25(4):89-93. doi: 10.3969/j.issn.1672-9897.2011.04.017
  • 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

    Figures(13)  / Tables(1)

    Article Metrics

    Article views (807) PDF downloads(64) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return