Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites

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Izvoz citacije: ABNT
ILIĆ, Ivana ;PETROVIC, Zlatko ;MAKSIMOVIĆ, Mirko ;STUPAR, Slobodan ;STAMENKOVIĆ, Dragi .
Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites. 
Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 58, n.9, p. 553-559, june 2018. 
ISSN 0039-2480.
Available at: <https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/>. Date accessed: 17 sep. 2021. 
doi:http://dx.doi.org/10.5545/sv-jme.2011.157.
Ilić, I., Petrovic, Z., Maksimović, M., Stupar, S., & Stamenković, D.
(2012).
Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites.
Strojniški vestnik - Journal of Mechanical Engineering, 58(9), 553-559.
doi:http://dx.doi.org/10.5545/sv-jme.2011.157
@article{sv-jmesv-jme.2011.157,
	author = {Ivana  Ilić and Zlatko  Petrovic and Mirko  Maksimović and Slobodan  Stupar and Dragi  Stamenković},
	title = {Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {58},
	number = {9},
	year = {2012},
	keywords = {Composites; Failure analysis; FEM; Contact problem; Pin-loaded joints; Failure Index},
	abstract = {This paper considers a computation method in failure analysis of layered composites containing pin-loaded holes. The investigation is focused on developing a reliable computation procedure to analyze initial failure load for pin-loaded holes at layered composite structures. Finite element method (FEM) is used to determine stress distribution around the fastener hole. Combining Chang-Scott-Springer characteristic curve model and Tsai-Wu initial failure criterion are used to determine joint failure. Special attention in this work is paid to pin-load distributions and its effect on the load level of failure and its location. In previous work initial failure analysis was carried out using cosine distribution between pin/lug mechanically fastened joint. Here contact finite element pin/lug model is analysed. The influence of stacking sequences of layered composites containing pin-loaded holes is also investigated. Special attention is paid to failure load and mode analyses in composites with stacking sequence [0/(±45)3/903]S. The computation results are compared with available experimental results. Good correlations between computation and experimental results are obtained.},
	issn = {0039-2480},	pages = {553-559},	doi = {10.5545/sv-jme.2011.157},
	url = {https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/}
}
Ilić, I.,Petrovic, Z.,Maksimović, M.,Stupar, S.,Stamenković, D.
2012 June 58. Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 58:9
%A Ilić, Ivana 
%A Petrovic, Zlatko 
%A Maksimović, Mirko 
%A Stupar, Slobodan 
%A Stamenković, Dragi 
%D 2012
%T Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites
%B 2012
%9 Composites; Failure analysis; FEM; Contact problem; Pin-loaded joints; Failure Index
%! Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites
%K Composites; Failure analysis; FEM; Contact problem; Pin-loaded joints; Failure Index
%X This paper considers a computation method in failure analysis of layered composites containing pin-loaded holes. The investigation is focused on developing a reliable computation procedure to analyze initial failure load for pin-loaded holes at layered composite structures. Finite element method (FEM) is used to determine stress distribution around the fastener hole. Combining Chang-Scott-Springer characteristic curve model and Tsai-Wu initial failure criterion are used to determine joint failure. Special attention in this work is paid to pin-load distributions and its effect on the load level of failure and its location. In previous work initial failure analysis was carried out using cosine distribution between pin/lug mechanically fastened joint. Here contact finite element pin/lug model is analysed. The influence of stacking sequences of layered composites containing pin-loaded holes is also investigated. Special attention is paid to failure load and mode analyses in composites with stacking sequence [0/(±45)3/903]S. The computation results are compared with available experimental results. Good correlations between computation and experimental results are obtained.
%U https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/
%0 Journal Article
%R 10.5545/sv-jme.2011.157
%& 553
%P 7
%J Strojniški vestnik - Journal of Mechanical Engineering
%V 58
%N 9
%@ 0039-2480
%8 2018-06-28
%7 2018-06-28
Ilić, Ivana, Zlatko  Petrovic, Mirko  Maksimović, Slobodan  Stupar, & Dragi  Stamenković.
"Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites." Strojniški vestnik - Journal of Mechanical Engineering [Online], 58.9 (2012): 553-559. Web.  17 Sep. 2021
TY  - JOUR
AU  - Ilić, Ivana 
AU  - Petrovic, Zlatko 
AU  - Maksimović, Mirko 
AU  - Stupar, Slobodan 
AU  - Stamenković, Dragi 
PY  - 2012
TI  - Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites
JF  - Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2011.157
KW  - Composites; Failure analysis; FEM; Contact problem; Pin-loaded joints; Failure Index
N2  - This paper considers a computation method in failure analysis of layered composites containing pin-loaded holes. The investigation is focused on developing a reliable computation procedure to analyze initial failure load for pin-loaded holes at layered composite structures. Finite element method (FEM) is used to determine stress distribution around the fastener hole. Combining Chang-Scott-Springer characteristic curve model and Tsai-Wu initial failure criterion are used to determine joint failure. Special attention in this work is paid to pin-load distributions and its effect on the load level of failure and its location. In previous work initial failure analysis was carried out using cosine distribution between pin/lug mechanically fastened joint. Here contact finite element pin/lug model is analysed. The influence of stacking sequences of layered composites containing pin-loaded holes is also investigated. Special attention is paid to failure load and mode analyses in composites with stacking sequence [0/(±45)3/903]S. The computation results are compared with available experimental results. Good correlations between computation and experimental results are obtained.
UR  - https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/
@article{{sv-jme}{sv-jme.2011.157},
	author = {Ilić, I., Petrovic, Z., Maksimović, M., Stupar, S., Stamenković, D.},
	title = {Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites},
	journal = {Strojniški vestnik - Journal of Mechanical Engineering},
	volume = {58},
	number = {9},
	year = {2012},
	doi = {10.5545/sv-jme.2011.157},
	url = {https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/}
}
TY  - JOUR
AU  - Ilić, Ivana 
AU  - Petrovic, Zlatko 
AU  - Maksimović, Mirko 
AU  - Stupar, Slobodan 
AU  - Stamenković, Dragi 
PY  - 2018/06/28
TI  - Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites
JF  - Strojniški vestnik - Journal of Mechanical Engineering; Vol 58, No 9 (2012): Strojniški vestnik - Journal of Mechanical Engineering
DO  - 10.5545/sv-jme.2011.157
KW  - Composites, Failure analysis, FEM, Contact problem, Pin-loaded joints, Failure Index
N2  - This paper considers a computation method in failure analysis of layered composites containing pin-loaded holes. The investigation is focused on developing a reliable computation procedure to analyze initial failure load for pin-loaded holes at layered composite structures. Finite element method (FEM) is used to determine stress distribution around the fastener hole. Combining Chang-Scott-Springer characteristic curve model and Tsai-Wu initial failure criterion are used to determine joint failure. Special attention in this work is paid to pin-load distributions and its effect on the load level of failure and its location. In previous work initial failure analysis was carried out using cosine distribution between pin/lug mechanically fastened joint. Here contact finite element pin/lug model is analysed. The influence of stacking sequences of layered composites containing pin-loaded holes is also investigated. Special attention is paid to failure load and mode analyses in composites with stacking sequence [0/(±45)3/903]S. The computation results are compared with available experimental results. Good correlations between computation and experimental results are obtained.
UR  - https://www.sv-jme.eu/sl/article/computation-method-in-failure-analysis-of-mechanically-fastened-joints-at-layered-composites/
Ilić, Ivana, Petrovic, Zlatko, Maksimović, Mirko, Stupar, Slobodan, AND Stamenković, Dragi.
"Computation Method in Failure Analysis of Mechanically Fastened Joints at Layered Composites" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 58 Number 9 (28 June 2018)

Avtorji

Inštitucije

  • Military Technical Institute, Serbia 1
  • Faculty of Mechanical Engineering in Belgrade, Serbia 2
  • Water Supplies, Serbia 3
  • Termoelektro, Serbia 4

Informacije o papirju

Strojniški vestnik - Journal of Mechanical Engineering 58(2012)9, 553-559

https://doi.org/10.5545/sv-jme.2011.157

This paper considers a computation method in failure analysis of layered composites containing pin-loaded holes. The investigation is focused on developing a reliable computation procedure to analyze initial failure load for pin-loaded holes at layered composite structures. Finite element method (FEM) is used to determine stress distribution around the fastener hole. Combining Chang-Scott-Springer characteristic curve model and Tsai-Wu initial failure criterion are used to determine joint failure. Special attention in this work is paid to pin-load distributions and its effect on the load level of failure and its location. In previous work initial failure analysis was carried out using cosine distribution between pin/lug mechanically fastened joint. Here contact finite element pin/lug model is analysed. The influence of stacking sequences of layered composites containing pin-loaded holes is also investigated. Special attention is paid to failure load and mode analyses in composites with stacking sequence [0/(±45)3/903]S. The computation results are compared with available experimental results. Good correlations between computation and experimental results are obtained.

Composites; Failure analysis; FEM; Contact problem; Pin-loaded joints; Failure Index