LIFTING SURFACE THEORY OF AXIAL COMPRESSOR BLADE ROWS .1. SUBSONIC COMPRESSOR

被引：12
作者：
OKUROUNM.O
MCCUNE, JE
机构：
[1] UNIV LAGOS,LAGOS,NIGERIA
[2] MIT,CAMBRIDGE,MA
来源：
AIAA JOURNAL | 1974年 / 12卷 / 10期
关键词：
D O I：
10.2514/3.49491
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：1363 / 1372
页数：10
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