PREDICTION OF UNSTEADY AIRLOADS FOR OBLIQUE BLADE-GUST INTERACTION IN COMPRESSIBLE FLOW

被引：4

作者：

CHU, S ^{[1
]}

WIDNALL, SE ^{[1
]}

机构：

[1] MIT,DEPT AERON & ASTRONAUT,CAMBRIDGE,MA

来源：

AIAA JOURNAL | 1974年 / 12卷 / 09期

关键词：

D O I：

10.2514/3.49458

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1228 / 1235

页数：8

共 13 条

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[8]

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[10] UNSTEADY THIN-AIRFOIL THEORY FOR SUBSONIC FLOW [J].

OSBORNE, C .

AIAA JOURNAL, 1973, 11 (02) :205-209

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