CLOSED FORM SOLUTIONS FOR THE INTERLAMINAR STRESS-FIELD IN ANGLE-PLY AND CROSS-PLY LAMINATES

被引：80

作者：

KASSAPOGLOU, C ^{[1
]}

LAGACE, PA ^{[1
]}

机构：

[1] MIT,DEPT AERONAUT & ASTRONAUT,TECHNOL LAB ADV COMPOSITES,CAMBRIDGE,MA 02139

来源：

JOURNAL OF COMPOSITE MATERIALS | 1987年 / 21卷 / 04期

关键词：

D O I：

10.1177/002199838702100401

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

引用

页码：292 / 308

页数：17

共 9 条

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[2]

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[8] BOUNDARY-LAYER EFFECTS IN COMPOSITE LAMINATES .1. FREE-EDGE STRESS SINGULARITIES [J].

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