1999
DOI: 10.1080/107594199305502
|View full text |Cite
|
Sign up to set email alerts
|

Failure Analysis of Two-Dimensional Carbon-Epoxy Composite Plate Pinned Joint

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

1
27
0

Year Published

2007
2007
2023
2023

Publication Types

Select...
7

Relationship

0
7

Authors

Journals

citations
Cited by 47 publications
(29 citation statements)
references
References 14 publications
1
27
0
Order By: Relevance
“…14- 16, respectively. For K/D = 3, the mean value of the failure load is 7% higher than that of the immersed specimens under M = 0.…”
Section: Resultsmentioning
confidence: 97%
See 1 more Smart Citation
“…14- 16, respectively. For K/D = 3, the mean value of the failure load is 7% higher than that of the immersed specimens under M = 0.…”
Section: Resultsmentioning
confidence: 97%
“…They concluded that ultimate load capacity depends on E/D, S/D and P/D ratios. Aktas and Karakuzu [16] have carried out a failure analysis of a mechanically fastened carbon-fiber reinforced epoxy composite plate of arbitrary orientation. In that work, failure load and failure mode have been analyzed experimentally and numerically using Tsai-Hill and fiber tensile-compressive failure criteria.…”
Section: Introductionmentioning
confidence: 99%
“…Aktas ß and Karakuzu [5] worked on pin connections of continuous fibre reinforced epoxy composite laminates, investigated the loading, which causes damage on the connections, and the failure types experimentally and numerically. Chang and Scott [6] investigated the laminates, which are fibers reinforced having different layers and different configurations.…”
Section: Introductionmentioning
confidence: 99%
“…It has been observed in an experiment that mechanically fastened joints fail in three basic failure modes: net-tension, shear-out, and bearing [1][2][3][4][5][6][7][8][9][10][11][12][13][14][15][16][17][18][19][20]. Typical damage caused by each mode is shown in Figure 5.…”
Section: Experimental Studymentioning
confidence: 99%
“…Parametric studies were performed experimentally for determining effects of joint geometry and fiber orientation on the failure strength and failure mode. Aktas and Karakuzu [5] carried out a failure analysis of mechanically fastened joints on arbitrary oriented carbon fiber reinforced epoxy composite plate. The failure loads and failure modes were analyzed experimentally and numerically using Tsai-Hill and fiber tensile-compressive failure criteria.…”
Section: Introductionmentioning
confidence: 99%