NONLINEAR MULTIMODE RESPONSE OF CLAMPED RECTANGULAR-PLATES TO ACOUSTIC LOADING

被引：12

作者：

MEI, C ^{[1
]}

PAUL, DB ^{[1
]}

机构：

[1] USAF,WRIGHT AERONAUT LABS,FLIGHT DYNAM LAB,STRUCT INTEGR BRANCH,WRIGHT PATTERSON AFB,OH 45433

来源：

AIAA JOURNAL | 1986年 / 24卷 / 04期

关键词：

D O I：

10.2514/3.9320

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：643 / 648

页数：6

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