2020
DOI: 10.1016/j.matpr.2020.02.582
|View full text |Cite
|
Sign up to set email alerts
|

Computational stress analysis of Chicken Feather Fibre (CFF) with Epoxy-Resin matrix composite material

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
2
1

Citation Types

0
3
0

Year Published

2020
2020
2024
2024

Publication Types

Select...
7
1

Relationship

0
8

Authors

Journals

citations
Cited by 9 publications
(3 citation statements)
references
References 5 publications
0
3
0
Order By: Relevance
“…To ensure the safety of the new constructs, it is necessary to choose allowable stresses and restrict the applied load to a lower value than the construct can fully support ( Casavola et al, 2011 ; Badalassi et al, 2014 ; Deng et al, 2021 ). Considering the inescapable microcracks of the implant and crack growth, allowable stress is a powerful instrument for assessing the implant in terms of strength theory and suitability of the metal material ( Gross and Abel 2001 ; Sarma and Adeli 2005 ; Manral et al, 2020 ). Considering defects in the implant material and the influence of processing technology, greater design load and safe allowable stress should be adopted in the biomechanical assessment of screw failure risk ( Agius et al, 2018 ; Anitua et al, 2018 ; Rahimizadeh et al, 2018 ; Choi et al, 2019 ).…”
Section: Discussionmentioning
confidence: 99%
“…To ensure the safety of the new constructs, it is necessary to choose allowable stresses and restrict the applied load to a lower value than the construct can fully support ( Casavola et al, 2011 ; Badalassi et al, 2014 ; Deng et al, 2021 ). Considering the inescapable microcracks of the implant and crack growth, allowable stress is a powerful instrument for assessing the implant in terms of strength theory and suitability of the metal material ( Gross and Abel 2001 ; Sarma and Adeli 2005 ; Manral et al, 2020 ). Considering defects in the implant material and the influence of processing technology, greater design load and safe allowable stress should be adopted in the biomechanical assessment of screw failure risk ( Agius et al, 2018 ; Anitua et al, 2018 ; Rahimizadeh et al, 2018 ; Choi et al, 2019 ).…”
Section: Discussionmentioning
confidence: 99%
“…Due to the prominent combination of low shrinkage, dimensional stability, adhesion, dielectric properties, and processing versatility, epoxies are the most common thermosetting polymer for high-performance composites and adhesives [1][2][3]. Furthermore, epoxy has good moisture resistance and is the best material for heavy-duty coatings application due to its superior toughness and hardness values [4,5] Nevertheless, its rigidity, brittleness, and poor resistance to crack propagation limit its applications [6]. Many attempts have been made to improve their physical properties by a variety of methods, including adding nanoparticles to polymer composite [7].…”
Section: Introductionmentioning
confidence: 99%
“…Recent publications on the waste feathers' application for composite materials development report mainly on the combination of waste feathers with synthetic polymers such as polylactide, polyethylene, epoxy-resin, polyurethane, etc. [5,[18][19][20][21][22][23]. In all these investigations synthetic polymers represent one of the main components, and the proportion of waste feathers in composite materials is rather low (below 10%).…”
Section: Introductionmentioning
confidence: 99%