UNSTEADY-FLOW ABOUT POROUS CHAMBERED SHELLS

被引:6
|
作者
SARPKAYA, T
LINDSEY, PJ
机构
[1] Naval Postgraduate School, Monterey, CA
来源
JOURNAL OF AIRCRAFT | 1991年 / 28卷 / 08期
关键词
D O I
10.2514/3.46055
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A numerical simulation was carried out through the use of the vortex-element methods to investigate the characteristics of an impulsively started uniform flow, decelerating at prescribed rates about a two-dimensional cambered porous shell, with an included angle of 120 deg, for the purpose of understanding the effects of porosity on the conditions under which wake recontact occurs.
引用
收藏
页码:502 / 508
页数:7
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