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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