EFFECT OF A FUSELAGE ON DELTA-WING VORTEX BREAKDOWN

被引：9
|
作者：
STRAKA, WA
HEMSCH, MJ
机构：
[1] George Washington University, Hampton, VA
[2] Lockheed Engineering and Sciences Company, Hampton, VA
来源：
JOURNAL OF AIRCRAFT | 1994年 / 31卷 / 04期
关键词：
D O I：
10.2514/3.46600
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：1002 / 1005
页数：4
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