DESIGN OF SUPERCRITICAL SWEPT WINGS

被引：46
作者：
GARABEDIAN, P
MCFADDEN, G
机构：
来源：
AIAA JOURNAL | 1982年 / 20卷 / 03期
关键词：
AERODYNAMICS - Wings and Airfoils;
D O I：
10.2514/3.7912
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
A computational method to design supercritical swept wings is discussed that is based on a well-posed free boundary problem for the velocity potential. An improved formula for the wave drag is included.
引用
收藏
页码：289 / 291
页数：3
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