Advanced Search
Volume 31 Issue 04
Apr.  2005
Turn off MathJax
Article Contents
Abstract
References
Journal of Beijing University of Aeronautics and Astronautics  > 2005  >  31(04): 459-463.
Jiang Qideng. Flight test of high sink speed symmetric landing used in land-based aircraft strength verification[J]. Journal of Beijing University of Aeronautics and Astronautics, 2013, 39(11): 1421-1425. (in Chinese)
Citation: Hao Weidong, Deng Xueying, Qu Fanglianget al. Simulated test technique for engine air intake and exhaust in high speed wind tunnel[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(04): 459-463. (in Chinese)
shu

Simulated test technique for engine air intake and exhaust in high speed wind tunnel

  • 1.

    School of Aeronautic Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • 2. Chinese Aerodynamic Research Institute of Aeronautics, Harbin 150001,China

  • Received Date: 14 Oct 2003
  • Publish Date: 30 Apr 2005
    Abstract
  • To study this test technique, the engine simulator(turbine powered simulator, ejectors)and the simulated parameters were analyzed and compared firstly in this paper. The Calculating methods of the ejector were presented using the theoretical base of One-dimensional ideal flow. An engine air intake and exhaust simulation experiment of a cruise missile with the ejector(the maximum diameter of the ejector is 41mm) was conducted in the FL-7 transonic wind tunnel.The test results showed that the free stream Mach number and nozzle pressure ratio getting 100% simulated, the flux coefficient realizing 89% simulated. The air intake and exhaust can increase the value of lift and drag, simultaneously the value of pitching moment was decreased, the value of base drag of the model is negative in no matter which situation whether existing air intake and exhaust or not.

     

    • FullText(HTML)
    • References(1)
  • [1] 起麟.风洞试验[M].北京:国防工业出版社,2000.295~305 Yun Qilin. Wind tunnel testing [M]. Beijing:National Defence Industry Press,2000. 295~305 (in Chinese) [2] 卫东,曲芳亮.校准箱的基本结构和应用[J].流体力学试验与测量,2002,16(4):27~32 Hao Weidong, Qu Fangliang. The basic construction and use of the calibration tank[J]. Experiments and Measurements in Fluid Mechanics, 2002,16(4):27~32(in Chinese) [3] 德馨.风洞天平〔M〕.北京:国防工业出版社,2001.225~225 He Dexin. Wind tunnel balance [M].Beijing:National Defence Industry Press, 2001.225~225(in Chinese) [4] 洁川.风洞试验手册[M].北京:航空工业出版社,2002.369~377 Fan Jiechuan. Handbook of wind tunnel test[M]. Beijing:Aeronautics Industry Press, 2002.369~377(in Chinese)
    • 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(3646) PDF downloads(1162) 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