VORTEX SHEET SHORTENING IN THE SMITH MODEL FOR SLENDER DELTA WINGS WITH LEADING-EDGE SEPARATION

被引：0

作者：

LAMMLEIN, S ^{[1
]}

WAGNER, B ^{[1
]}

机构：

[1] DORNIER GMBH,THEORET AERODYNAM ABT,D-7990 FRIEDRICHSHAFEN 1,FED REP GER

来源：

ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1983年 / 7卷 / 04期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：279 / 281

页数：3

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