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Numerical Investigation of Aerodynamic Characteristics for Multi-Fin Rockets/Missiles
Author(s): 
Pages: 686-689
Year: Issue:  6
Journal: TRANSACTIONS OF BEIJING INSTITUTE OF TECHNOLOGY

Keyword:  多片尾翼布局弹箭气动外形气动特性数值模拟;
Abstract: 用数值模拟方法研究多片尾翼布局弹箭的气动特性.以三维Navier-Stokes方程为控制方程,用CFD方法对4片、6片与8片平直形尾翼和卷弧形尾翼弹箭的流场进行数值模拟研究,得到的气动特性结果与风洞实验结果基本吻合,为多片尾翼布局弹箭的气动设计及尾翼片数的合理选择提供了依据.
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