FLUTTER ANALYSIS OF MISSILE CONTROL SURFACES CONTAINING STRUCTURAL NONLINEARITIES

被引：48
作者：
LAURENSON, RM
TRN, RM
机构：
来源：
AIAA JOURNAL | 1980年 / 18卷 / 10期
关键词：
D O I：
10.2514/3.50876
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
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页码：1245 / 1251
页数：7
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