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�������պ����ѧѧ�� 2002, Vol. 28 Issue (4) :395-398    DOI:
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Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations
HUANG Xian-lu, YAN Chao, CHEN Liang, LONG Yao-song*
Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics

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Abstract�� 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.
Keywords�� guided missiles   aerodynamics   computation fluid dynamics     
Received 2000-10-24;
About author: ����»(1975-),��,����������,˶ʿ��,100083,����.
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����», �ֳ�, ����, ��Ң��.��������������������������ֵ����[J]  �������պ����ѧѧ��, 2002,V28(4): 395-398
HUANG Xian-lu, YAN Chao, CHEN Liang, LONG Yao-song.Numerical Analysis of Complex Flowfields Around Multi-Wing Missiles and Its Aerodynamic Force Computations[J]  JOURNAL OF BEIJING UNIVERSITY OF AERONAUTICS AND A, 2002,V28(4): 395-398
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