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
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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
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页码：279 / 281
页数：3
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