Bearing strength of carbon epoxy laminates under static and dynamic loading

被引:35
作者
Aktas, A [1 ]
机构
[1] Afyon Kocatepe Univ, Dept Mech Engn, Usak, Turkey
关键词
carbon fibre; fatigue; S-N fatigue curve; laminate mechanics; joints;
D O I
10.1016/j.compstruct.2004.02.007
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
An experimental study has been carried out to investigate both the static and dynamic bearing strengths of a pinned-joint carbon epoxy composite plate with [0degrees/45degrees/-45degrees/90degrees]s and [90degrees/45degrees/-45degrees/0degrees]s stacking configurations. The static and dynamic experiments have been carried out according to the ASTM D953 standards and ASTM STP 749, respectively [ASTM D 953-D, Standard Test method for Bearing Strength of Plastics, ASTM Designation. 342; Joining of Composite Materials, ASTM STP 749, American Society for Testing and Materials (1981) 131]. The ratio of the edge distance to the pin diameter (E/D), and that of the width to the pin diameter (W/D) of the specimens were varied to obtain the static bearing strength and the S-N fatigue curve. The experiments show that the static bearing strengths reach their upper limit when E/D and W/D ratios are equal to or greater than 4 for both [0degrees/ 45degrees/-45degrees/90degrees]s and [90degrees/45degrees/-45degrees/0degrees]s stacking sequences. The fatigue strength, on the other hand, reduces by up to 65% as E/D and W/D ratios increase for both stacking configurations. Published by Elsevier Ltd.
引用
收藏
页码:485 / 489
页数:5
相关论文
共 12 条
[1]   BEARING STRENGTH OF AUTOCLAVE AND OVEN CURED KEVLAR EPOXY LAMINATES UNDER STATIC AND DYNAMIC LOADING [J].
AKAY, M ;
MUN, SKA .
COMPOSITES, 1995, 26 (06) :451-456
[2]   The effect of stacking sequence of carbon epoxy composite laminates on pinned-joint strength [J].
Aktas, A ;
Dirikolu, MH .
COMPOSITE STRUCTURES, 2003, 62 (01) :107-111
[3]   Failure analysis of two-dimensional carbon-epoxy composite plate pinned joint [J].
Aktas, A ;
Karakuzu, R .
MECHANICS OF COMPOSITE MATERIALS AND STRUCTURES, 1999, 6 (04) :347-361
[4]  
*ASTM, 953D ASTM, P342
[5]   FAILURE STRENGTH OF NONLINEARLY ELASTIC COMPOSITE LAMINATES CONTAINING A PIN LOADED HOLE [J].
CHANG, FK ;
SCOTT, RA ;
SPRINGER, GS .
JOURNAL OF COMPOSITE MATERIALS, 1984, 18 (05) :464-477
[6]   ON THE BEARING STRENGTHS OF CFRP LAMINATES [J].
COLLINGS, TA .
COMPOSITES, 1982, 13 (03) :241-252
[7]  
Crews JHJ, 1981, ASTM STP, P131
[8]   FATIGUE BEHAVIOR OF CARBON-FIBER REINFORCED-PLASTICS [J].
HARRIS, B ;
REITER, H ;
ADAM, T ;
DICKSON, RF ;
FERNANDO, GF .
COMPOSITES, 1990, 21 (03) :232-242
[9]   FATIGUE FAILURE OF COMPOSITE BOLTED JOINTS [J].
HERRINGTON, PD ;
SABBAGHIAN, M .
JOURNAL OF COMPOSITE MATERIALS, 1993, 27 (05) :491-512
[10]   A study of the effects of various geometric parameters on the failure strength of pin-loaded woven-glass-fiber reinforced epoxy laminate [J].
Okutan, B ;
Aslan, Z ;
Karakuzu, R .
COMPOSITES SCIENCE AND TECHNOLOGY, 2001, 61 (10) :1491-1497