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: 09 dec. 2024. 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. 09 Dec. 2024
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)
Strojniški vestnik - Journal of Mechanical Engineering 58(2012)9, 553-559
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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.