Volume 28 Issue 4
Apr.  2002
Turn off MathJax
Article Contents
HUANG Xian-lu, YAN Chao, CHEN Liang, et al. Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4): 395-398. (in Chinese)
Citation: HUANG Xian-lu, YAN Chao, CHEN Liang, et al. Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4): 395-398. (in Chinese)

Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations

  • Received Date: 24 Oct 2000
  • Publish Date: 30 Apr 2002
  • The applications of modified Jameson's scheme to the complex flow around the missiles with canards and tails, result in good agreement between computations and experiment data of the standard missile model of U.S.A.. In computations, the latest modifications of Jameson's scheme are adopted to extend applications of the scheme to high supersonic and high Reynolds number flows. The multi-zone technique and 3-D elliptic grid generation method are also employed to precisely simulate the flows.

     

  • loading
  • [1] Ekaterinaris J A. Analysis of flowfields over missile configurations at subsonic speeds[J]. J of Spacecraft and Rockets,1995,32(3):385~391. [2]Streit Th. Euler and N-S solutions for supersonic flow around a complex missile[J]. J of Spacecraft and Rockets, 1994,31(4):600~608. [3]阎 超,陈 靓.球柱三维分离及涡流的数值模拟[J].航空学报, 1996,17(6):728~731. [4]Jameson A,Schmidt W,Turkel E.Numerical solutions of the Euler equations by finite volume methods using Runge-Kutta time-stepping schemes . AIAA Paper 81-1259,1981. [5] Martinelli L. Calculations of viscous flows with a multigrid method . Princeton:Princeton University, MAE Department, 1987. [6]Swanson R C,Turkel E. Artificial dissipation and central difference schemes for the Euler and Navier-Stokes equations . AIAA Paper 87-1107,1987. [7]Turkel E. Multigrid for hypersonic viscous two- and three-dimensional flows . AIAA Paper 91-2572-CP,1991. [8] 陈 靓,阎 超.喷流粘性数值模拟中的混合型远场边界效应研究[J].北京航空航天大学学报,1997,23(3):346~350. [9]Blair Jr A B. Experimental study of tail-span effects on canard-controlled missile[J]. Journal of Spacecraft and Rockets, 1993,30(5):635~640.
  • 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(3029) PDF downloads(914) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return