Advanced Search
Volume 26 Issue 3
Mar.  2000
Turn off MathJax
Article Contents
Journal of Beijing University of Aeronautics and Astronautics  > 2000  >  26(3): 340-343.
PENG Jing, JIN Chang-jiang. Research on the Numerical Simulation of Aircraft Carrier Air Wake[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(3): 340-343. (in Chinese)
Citation: PENG Jing, JIN Chang-jiang. Research on the Numerical Simulation of Aircraft Carrier Air Wake[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(3): 340-343. (in Chinese)
shu

Research on the Numerical Simulation of Aircraft Carrier Air Wake

  • Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

  • Received Date: 08 Dec 1998
  • Publish Date: 31 Mar 2000
    Abstract
  • A model of carrier air wake is selected to simulate the spatial distribution of velocity of air wake in MATLAB on a PC for study of environmental effects on approaching and landing of the carrier base aircraft. The air wake can be divided into four components according to their causes: the power spectra of the component of free random turbulence is simulated by means of shape filter; the steady component is acquired by linear interpolating; the periodic component is directly calculated; and the random turbulence induced by carrier is realized with SIMULINK Toolbox in MATLAB. The simulation shows that the periodic component is the dominant component of the air wake. The further validation of this model needs supports of more experimental data and data obtained aboard.

     

    • FullText(HTML)
  • loading
    • References(1)
  • [1] 飞行力学杂志社.军用规范——有人驾驶飞机的飞行品质(MIL-F-8785C)的背景资料和使用指南[S]. 陕西富平:飞行力学杂志社,1985. [2]肖业伦,金长江. 大气扰动中的飞行原理[M]. 北京:国防工业出版社,1993. 167~173. [3]Nave R L. Development and analysis of a CVA and a 1052 class fast frigate air wake model . ADA701622, 1976.6~13. [4]Powell F D, Theoclitus T. Study of an automatic carrier landing environment with the AN/SPN-10 landing control central . AD463348, 1965. 65~70. [5]赵震炎,肖业伦,施毅坚.　Dryden大气紊流模型的数字仿真技术[J].　航空学报,1986, 7(5):433~443. [6]Lehman A F. An experimental study of the dynamic and steady state flow disturbances encountered by aircraft during a carrier landing approach . AD606 886, 1965.
    • Relative Articles
    • Supplements(0)
    • Cited By
  • 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
    Get Citation
    PDF
    XML

    Article Metrics

    Article views(2760) PDF downloads(1318) Cited by()
    Proportional views
    Related

    Copyright © Journal of Beijing University of Aeronautics and Astronautics

    Address: Editorial Department of Journal of Beijing University of Aeronautics and Astronautics, 37 Xueyuan Road, Haidian District, Beijing Post Code: 100191 Email: jbuaa@buaa.edu.cn

    Supported by: Beijing Renhe Information Technology Co., Ltd.    

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return