FAILURE OF COMPOSITE LAMINATES CONTAINING PIN LOADED HOLES - METHOD OF SOLUTION

被引：126

作者：

CHANG, FK ^{[1
]}

SCOTT, RA ^{[1
]}

SPRINGER, GS ^{[1
]}

机构：

[1] STANFORD UNIV,DEPT AERONAUT & ASTRONAUT,STANFORD,CA 94305

来源：

JOURNAL OF COMPOSITE MATERIALS | 1984年 / 18卷 / 03期

关键词：

D O I：

10.1177/002199838401800305

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

引用

页码：255 / 278

页数：24

共 32 条

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[2]

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[3] STRENGTH OF MECHANICALLY FASTENED COMPOSITE JOINTS [J].

CHANG, FK ;

SCOTT, RA ;

SPRINGER, GS .

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[4] THE EFFECT OF LAMINATE CONFIGURATION ON CHARACTERISTIC LENGTHS AND RAIL SHEAR-STRENGTH [J].

CHANG, FK ;

SCOTT, RA ;

SPRINGER, GS .

JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (03) :290-296

[5] DESIGN OF COMPOSITE LAMINATES CONTAINING PIN LOADED HOLES [J].

CHANG, FK ;

SCOTT, RA ;

SPRINGER, GS .

JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (03) :279-289

[6] FAILURE OF COMPOSITE LAMINATES CONTAINING PIN LOADED HOLES - METHOD OF SOLUTION [J].

CHANG, FK ;

SCOTT, RA ;

SPRINGER, GS .

JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (03) :255-278

[7]

CHANG FK, 1982, AFWALTR824095 AIR FO

[8]

CHANG FK, 1984, AFWALTR844029 AIR FO

[9]

COLLINGS TA, 1982, COMPOSITES, V13, P242

[10]

COLLINGS TA, 1975, TR75127 BRIT ROYAL A

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