UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW

被引：28

|

作者：

OSBORNE, C ^{[1
]}

机构：

[1] CORNELL UNIV,ITHACA,NY 14850

来源：

AIAA JOURNAL | 1973年 / 11卷 / 02期

关键词：

D O I：

10.2514/3.6730

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：205 / 209

页数：5

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