LOW-REYNOLDS-NUMBER AIRFOIL DESIGN FOR THE MIT DAEDALUS PROTOTYPE - A CASE-STUDY

被引：44
|
作者：
DRELA, M
机构：
[1] MIT, United States
来源：
JOURNAL OF AIRCRAFT | 1988年 / 25卷 / 08期
关键词：
Light Eagle Airfoils - Low-Reynolds-Number Airfoil - MIT Daedalus Aircraft - Separation Bubble Control - Transitional Separation Bubbles - Viscous/Inviscid Interaction;
D O I：
10.2514/3.45650
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
(Edited Abstract)
引用
收藏
页码：724 / 732
页数：9
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