Wang Su, Zhou Feng, Zhang Yingliet al. Numerical simulation of intersection line welding in installation pedestal on aeroengine combustion chamber[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(8): 986-990. (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.

     

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