TRANSONIC PANEL METHOD TO DETERMINE LOADS ON OSCILLATING AIRFOILS WITH SHOCKS

被引：7
|
作者：
HOUNJET, MHL
机构：
来源：
AIAA JOURNAL | 1981年 / 19卷 / 05期
关键词：
D O I：
10.2514/3.50977
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：559 / 566
页数：8
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