Volume 23 Issue 10
Oct.  2008
Turn off MathJax
Article Contents
Article Navigation >  Journal of Aerospace Power  > 2008  >  23(10): 1882-1887
HU Li, CAO Yi-hua, ZHAO Ming. Numerical simulation of helicopter rotor-fuselage-engine aerodynamic interactions[J]. Journal of Aerospace Power, 2008, 23(10): 1882-1887.
Citation: HU Li, CAO Yi-hua, ZHAO Ming. Numerical simulation of helicopter rotor-fuselage-engine aerodynamic interactions[J]. Journal of Aerospace Power, 2008, 23(10): 1882-1887.
shu

Numerical simulation of helicopter rotor-fuselage-engine aerodynamic interactions

  • School of Aeronautical Science and Technology, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

  • Received Date: 2007-09-10
  • Rev Recd Date: 2008-04-28
  • Publish Date: 2008-10-28
    Abstract
  • The rotor-fuselage-engine aerodynamic interactions were studied using computational fluid dynamics numerical tools.The body-fitted structural grid was generated through multi-block grid technique.The finite volume method was adopted and incompressible Navier-Stokes equation was solved.The flow field and performance of the helicopter in forward flight were analyzed.Firstly,the accuracy of viscous simulation was investigated for the isolated fuselage configuration.Then,the rotor-fuselage aerodynamic interactions using the actuator disk model were obtained by discussing the influence of rotor on fuselage pressure distribution.Finally,the effect of the helicopter engine inlet and outlet was analyzed using a simplified engine model and the rotor-fuselage-engine interactions were obtained.

     

    • FullText(HTML)
  • loading
    • References(9)
  • [1]
    Cao Y,Yuan K,Li X.Computational methods for simulation of flow around helicopter engine inlet[J].Journal of Aircraft,2006,43(1):141-146.
    [2]
    Cao Y,Su Y.Insight into the effects of rotor downwash on engine jet[J].Aircraft Engineering and Aerospace Technology,2003,75(4):345-349.
    [3]
    Benoit B,Dequin A-M,Kampa K,et al.HOST,a general helicopter simulation,tool for Germany and France ER3.Virginia Beach(USA):56th Annual Forum of the Ameriean Helicopter Society,2000:1110-1131.
    [4]
    Khalid M,Sun Y.Numerical simulation of rotor-fuselage interaction[J].Canadian Aeronautics and Space Journal,1997,43(3):176-183.
    [5]
    Bettschart N.Rotor fuselage interaction:Euler and Navier-Stokes computations with an actuator disk[R].Montreal,Canada:American Helicopter Society 55th Annual Forum,1999:419-438.
    [6]
    Brezillon J.Simulation of rotor-fuselage interactions by Using an actuator diskrR].The Hague,Netherlands:26th European Rotorcraft Forum,2000,50:1-15.
    [7]
    Le Chuiton F.Actuator disc modeling for helicopter rotors[J].Aerospace Science and Technology,2004,8(4):285-297.
    [8]
    阎丽君.米-8/米-17系列直升机[M].北京:航空工业出版社,2006:155-159.
    [9]
    Renaud T,O'Brien D,Smith M,et al.Evaluation of isolated fuselage and rotor-fuselage interaction using CFD[R].Baltimore,MD:60th Annual Forum of the American Helicopter Society,2004:995-1009.
    • 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(2253.0KB)
    XML

    Article Metrics

    Article views (1762) PDF downloads(499) Cited by()
    Proportional views
    Related

    Copyright © 《Journal of Aerospace Power》 All Rights Reserved.

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

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return