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
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页码:502 / 508
页数:7
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