A GALERKIN TYPE FINITE-ELEMENT METHOD FOR ROTARY-WING AEROELASTICITY IN HOVER AND FORWARD FLIGHT

被引：0

作者：

STRAUB, FK ^{[1
]}

FRIEDMANN, PP ^{[1
]}

机构：

[1] UNIV CALIF LOS ANGELES, DEPT MECH & STRUCT, LOS ANGELES, CA 90024 USA

来源：

VERTICA | 1981年 / 5卷 / 01期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：75 / 98

页数：24

共 50 条

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