COMPARISON OF SUPERCRITICAL AIRFOIL FLOW CALCULATIONS WITH WIND-TUNNEL RESULTS

被引：0
|
作者：
KING, LS
JOHNSON, DA
机构：
[1] NASA, Ames Research Cent, Moffett, Field, CA, USA, NASA, Ames Research Cent, Moffett Field, CA, USA
来源：
AIAA JOURNAL | 1985年 / 23卷 / 09期
关键词：
D O I：
10.2514/3.9085
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
18
引用
收藏
页码：1301 / 1307
页数：7
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