COMPUTATIONAL SIMULATION OF VORTEX GENERATOR EFFECTS ON TRANSONIC SHOCK BOUNDARY-LAYER INTERACTION

被引：5

|

作者：

INGER, GR

SIEBERSMA, T

机构：

来源：

JOURNAL OF AIRCRAFT | 1989年 / 26卷 / 08期

关键词：

D O I：

10.2514/3.45826

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

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页码：697 / 698

页数：2

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