FLEXURAL FATIGUE OF CARBON FIBER-REINFORCED PEEK LAMINATES

被引：19

作者：

BUGGY, M

DILLON, G

机构：

[1] MIT,MFG & PROD LAB,CAMBRIDGE,MA 02139

[2] UNIV LIMERICK,DEPT MAT ENGN & IND CHEM,LIMERICK,IRELAND

[3] MIT,IND COMPOSITES & POLYMER PROC PROGRAM,CAMBRIDGE,MA 02139

来源：

COMPOSITES | 1991年 / 22卷 / 03期

关键词：

COMPOSITE MATERIALS; FLEXURAL FATIGUE; S-N CURVES; FATIGUE MODULUS DEGRADATION; WEIBULL ANALYSIS; CARBON FIBERS; PEEK; EPOXY RESIN;

D O I：

10.1016/0010-4361(91)90318-B

中图分类号：

TB33 [复合材料];

学科分类号：

摘要：

Stress/number of cycles to failure relations were established for unidirectional, cross-plied and angle-plied laminates of APC-2 using three-point bend flexure tests. Results for constant stress ratio fatigue tests were modelled using both Weibull and fatigue modulus degradation analyses. Behaviour was compared with that of an established carbon/epoxy system.

引用

页码：191 / 198

页数：8

共 16 条

[1]

[Anonymous], 1987, FATIGUE COMPOSITE MA

[2] FATIGUE TESTING OF MULTI-ANGLE LAMINATES OF CF/PEEK [J].