DAMAGE TOLERANT DESIGN USING COLLAPSE TECHNIQUES

被引：5

作者：

HAFTKA, RT

机构：

来源：

AIAA JOURNAL | 1983年 / 21卷 / 10期

关键词：

D O I：

10.2514/3.8268

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1462 / 1466

页数：5

共 15 条

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HAFTKA, RT ;

STARNES, JH .

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[8]

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[9] SENSITIVITY OF OPTIMUM SOLUTIONS OF PROBLEM PARAMETERS [J].

SOBIESZCZANSKISOBIESKI, J ;

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AIAA JOURNAL, 1982, 20 (09) :1291-1299

[10] PRELIMINARY DESIGN OF COMPOSITE WINGS FOR BUCKLING, STRENGTH, AND DISPLACEMENT CONSTRAINTS [J].

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