VIBRATION MEASUREMENTS OF AN AIRPLANE FUSELAGE STRUCTURE .1. TURBULENT BOUNDARY-LAYER EXCITATION

被引：36

作者：

WILBY, JF

GLOYNA, FL

机构：

来源：

JOURNAL OF SOUND AND VIBRATION | 1972年 / 23卷 / 04期

关键词：

D O I：

10.1016/0022-460X(72)90503-2

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

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页码：443 / &

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