2015
DOI: 10.1002/pc.23584
|View full text |Cite
|
Sign up to set email alerts
|

A novel approach for design of fiber angle and layer number of composite plates

Abstract: The aim of this study is developing a new algorithm to design fiber angle and layer number of laminated composite plates. In this algorithm, fiber angles are determined using stress values and layer numbers are determined using maximum stress failure theory. Different design domains are used under different loading conditions and results are investigated to show the performance of the algorithm. Design time of composite materials is decreased and design performance is increased using this algorithm. More effec… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2

Citation Types

0
2
0
1

Year Published

2017
2017
2020
2020

Publication Types

Select...
6

Relationship

0
6

Authors

Journals

citations
Cited by 6 publications
(3 citation statements)
references
References 10 publications
0
2
0
1
Order By: Relevance
“…Göv 12 developed a new approach for optimization of fiber angle and layer number of composites. Using stress values and maximum stress failure theory, fiber angles and layer numbers were determined.…”
Section: Introductionmentioning
confidence: 99%
“…Göv 12 developed a new approach for optimization of fiber angle and layer number of composites. Using stress values and maximum stress failure theory, fiber angles and layer numbers were determined.…”
Section: Introductionmentioning
confidence: 99%
“…Aynı zamanda güçlendirilmiş bölgeler ve takviyenin optimal noktasal eğimi araştırılmıştır. Göv [5] tarafından kompozitlerin katman sayısı ve elyaf açısı optimizasyonu için yeni yaklaşım geliştirilmiştir. Kullanılan gerilme değeri ve maksimum gerilme kırılma teorisi ile elyaf açısı ve katman sayısı belirlenmiştir.…”
Section: Gi̇ri̇ş (Introduction)unclassified
“…Göv [15] performed a study to develop an algorithm to design layer and fiber number of the composite plate. stress values were used to determine fiber angle and maximum stress failure theory was used to obtain layer numbers.…”
mentioning
confidence: 99%