Extending slender wing theory to not so slender wings

被引：3
作者：
Traub, LW [1 ]
机构：
[1] Texas A&M Univ, Dept Aerosp Engn, College Stn, TX 77843 USA
来源：
JOURNAL OF AIRCRAFT | 2003年 / 40卷 / 02期
关键词：
D O I：
10.2514/2.3109
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A method was presented to extend the results from slender wing theory to delta wings of high aspect ratio. A correction to account for the finite chord of the wing was incorporated into the rate of change of the local additional apparent mass. Comparisons of the expressions with numerical and experimental data showed excellent agreement.
引用
收藏
页码：399 / 402
页数：4
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