Proposed inflow/outflow boundary condition for direct computation of aerodynamic sound

被引：223

作者：

Freund, JB

机构：

[1] Stanford University, Stanford, CA

[2] Department of Mechanical Engineering, Flow Physics Division

来源：

AIAA JOURNAL | 1997年 / 35卷 / 04期

关键词：

D O I：

10.2514/2.167

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：740 / 742

页数：3

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