STAMENKOVIĆ, Dragi ;MAKSIMOVIĆ, Katarina ;NIKOLIĆ-STANOJEVIĆ, Vera ;MAKSIMOVIĆ, Stevan ;STUPAR, Slobodan ;VASOVIĆ, Ivana . Fatigue Life Estimation of Notched Structural Components. Strojniški vestnik - Journal of Mechanical Engineering, [S.l.], v. 56, n.12, p. 846-852, october 2017. ISSN 0039-2480. Available at: <https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/>. Date accessed: 19 nov. 2024. doi:http://dx.doi.org/.
Stamenković, D., Maksimović, K., Nikolić-Stanojević, V., Maksimović, S., Stupar, S., & Vasović, I. (2010). Fatigue Life Estimation of Notched Structural Components. Strojniški vestnik - Journal of Mechanical Engineering, 56(12), 846-852. doi:http://dx.doi.org/
@article{.,
author = {Dragi Stamenković and Katarina Maksimović and Vera Nikolić-Stanojević and Stevan Maksimović and Slobodan Stupar and Ivana Vasović},
title = {Fatigue Life Estimation of Notched Structural Components},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {56},
number = {12},
year = {2010},
keywords = {Notched structural components; lugs; analytic stress intensity factor of lugs; finite elements; X-FEM; fatigue life estimation; },
abstract = {This work considers the analytical/numerical methods and procedures for obtaining the stress intensity factors and for predicting the fatigue crack growth life of notched structural components. Many efforts have been made during the past two decades to evaluate the stress intensity factor for corner cracks and for through cracks emanating from fastener holes. A variety of methods have been used to estimate the stress intensity factor (SIF), values, such as approximate analytical methods, finite element method (FEM), finite element alternating, weight function, photo elasticity and fatigue tests. In this paper the analytic/numerical methods and procedures were used to obtain SIF, and predict the fatigue crack growth life for cracks at attachment lugs. Single through crack in the attachment lug analysis is considered. For this purpose analytic expressions are evaluated for SIF of cracked lug structures. For validation of the analytic stress intensity factors of cracked lugs, FEM with singular finite elements is used. Good agreement between computation and experimental results for fatigue life of aircraft cracked lugs was obtained. To determine crack trajectory of cracked structural components under mixed modes,, conventional singular finite elements and X-FEM are used.},
issn = {0039-2480}, pages = {846-852}, doi = {},
url = {https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/}
}
Stamenković, D.,Maksimović, K.,Nikolić-Stanojević, V.,Maksimović, S.,Stupar, S.,Vasović, I. 2010 October 56. Fatigue Life Estimation of Notched Structural Components. Strojniški vestnik - Journal of Mechanical Engineering. [Online] 56:12
%A Stamenković, Dragi %A Maksimović, Katarina %A Nikolić-Stanojević, Vera %A Maksimović, Stevan %A Stupar, Slobodan %A Vasović, Ivana %D 2010 %T Fatigue Life Estimation of Notched Structural Components %B 2010 %9 Notched structural components; lugs; analytic stress intensity factor of lugs; finite elements; X-FEM; fatigue life estimation; %! Fatigue Life Estimation of Notched Structural Components %K Notched structural components; lugs; analytic stress intensity factor of lugs; finite elements; X-FEM; fatigue life estimation; %X This work considers the analytical/numerical methods and procedures for obtaining the stress intensity factors and for predicting the fatigue crack growth life of notched structural components. Many efforts have been made during the past two decades to evaluate the stress intensity factor for corner cracks and for through cracks emanating from fastener holes. A variety of methods have been used to estimate the stress intensity factor (SIF), values, such as approximate analytical methods, finite element method (FEM), finite element alternating, weight function, photo elasticity and fatigue tests. In this paper the analytic/numerical methods and procedures were used to obtain SIF, and predict the fatigue crack growth life for cracks at attachment lugs. Single through crack in the attachment lug analysis is considered. For this purpose analytic expressions are evaluated for SIF of cracked lug structures. For validation of the analytic stress intensity factors of cracked lugs, FEM with singular finite elements is used. Good agreement between computation and experimental results for fatigue life of aircraft cracked lugs was obtained. To determine crack trajectory of cracked structural components under mixed modes,, conventional singular finite elements and X-FEM are used. %U https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/ %0 Journal Article %R %& 846 %P 7 %J Strojniški vestnik - Journal of Mechanical Engineering %V 56 %N 12 %@ 0039-2480 %8 2017-10-24 %7 2017-10-24
Stamenković, Dragi, Katarina Maksimović, Vera Nikolić-Stanojević, Stevan Maksimović, Slobodan Stupar, & Ivana Vasović. "Fatigue Life Estimation of Notched Structural Components." Strojniški vestnik - Journal of Mechanical Engineering [Online], 56.12 (2010): 846-852. Web. 19 Nov. 2024
TY - JOUR AU - Stamenković, Dragi AU - Maksimović, Katarina AU - Nikolić-Stanojević, Vera AU - Maksimović, Stevan AU - Stupar, Slobodan AU - Vasović, Ivana PY - 2010 TI - Fatigue Life Estimation of Notched Structural Components JF - Strojniški vestnik - Journal of Mechanical Engineering DO - KW - Notched structural components; lugs; analytic stress intensity factor of lugs; finite elements; X-FEM; fatigue life estimation; N2 - This work considers the analytical/numerical methods and procedures for obtaining the stress intensity factors and for predicting the fatigue crack growth life of notched structural components. Many efforts have been made during the past two decades to evaluate the stress intensity factor for corner cracks and for through cracks emanating from fastener holes. A variety of methods have been used to estimate the stress intensity factor (SIF), values, such as approximate analytical methods, finite element method (FEM), finite element alternating, weight function, photo elasticity and fatigue tests. In this paper the analytic/numerical methods and procedures were used to obtain SIF, and predict the fatigue crack growth life for cracks at attachment lugs. Single through crack in the attachment lug analysis is considered. For this purpose analytic expressions are evaluated for SIF of cracked lug structures. For validation of the analytic stress intensity factors of cracked lugs, FEM with singular finite elements is used. Good agreement between computation and experimental results for fatigue life of aircraft cracked lugs was obtained. To determine crack trajectory of cracked structural components under mixed modes,, conventional singular finite elements and X-FEM are used. UR - https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/
@article{{}{.},
author = {Stamenković, D., Maksimović, K., Nikolić-Stanojević, V., Maksimović, S., Stupar, S., Vasović, I.},
title = {Fatigue Life Estimation of Notched Structural Components},
journal = {Strojniški vestnik - Journal of Mechanical Engineering},
volume = {56},
number = {12},
year = {2010},
doi = {},
url = {https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/}
}
TY - JOUR AU - Stamenković, Dragi AU - Maksimović, Katarina AU - Nikolić-Stanojević, Vera AU - Maksimović, Stevan AU - Stupar, Slobodan AU - Vasović, Ivana PY - 2017/10/24 TI - Fatigue Life Estimation of Notched Structural Components JF - Strojniški vestnik - Journal of Mechanical Engineering; Vol 56, No 12 (2010): Strojniški vestnik - Journal of Mechanical Engineering DO - KW - Notched structural components, lugs, analytic stress intensity factor of lugs, finite elements, X-FEM, fatigue life estimation, N2 - This work considers the analytical/numerical methods and procedures for obtaining the stress intensity factors and for predicting the fatigue crack growth life of notched structural components. Many efforts have been made during the past two decades to evaluate the stress intensity factor for corner cracks and for through cracks emanating from fastener holes. A variety of methods have been used to estimate the stress intensity factor (SIF), values, such as approximate analytical methods, finite element method (FEM), finite element alternating, weight function, photo elasticity and fatigue tests. In this paper the analytic/numerical methods and procedures were used to obtain SIF, and predict the fatigue crack growth life for cracks at attachment lugs. Single through crack in the attachment lug analysis is considered. For this purpose analytic expressions are evaluated for SIF of cracked lug structures. For validation of the analytic stress intensity factors of cracked lugs, FEM with singular finite elements is used. Good agreement between computation and experimental results for fatigue life of aircraft cracked lugs was obtained. To determine crack trajectory of cracked structural components under mixed modes,, conventional singular finite elements and X-FEM are used. UR - https://www.sv-jme.eu/sl/article/fatigue-life-estimation-of-notched-structural-components/
Stamenković, Dragi, Maksimović, Katarina, Nikolić-Stanojević, Vera, Maksimović, Stevan, Stupar, Slobodan, AND Vasović, Ivana. "Fatigue Life Estimation of Notched Structural Components" Strojniški vestnik - Journal of Mechanical Engineering [Online], Volume 56 Number 12 (24 October 2017)
Strojniški vestnik - Journal of Mechanical Engineering 56(2010)12, 846-852
© The Authors, CC-BY 4.0 Int. Change in copyright policy from 2022, Jan 1st.
This work considers the analytical/numerical methods and procedures for obtaining the stress intensity factors and for predicting the fatigue crack growth life of notched structural components. Many efforts have been made during the past two decades to evaluate the stress intensity factor for corner cracks and for through cracks emanating from fastener holes. A variety of methods have been used to estimate the stress intensity factor (SIF), values, such as approximate analytical methods, finite element method (FEM), finite element alternating, weight function, photo elasticity and fatigue tests. In this paper the analytic/numerical methods and procedures were used to obtain SIF, and predict the fatigue crack growth life for cracks at attachment lugs. Single through crack in the attachment lug analysis is considered. For this purpose analytic expressions are evaluated for SIF of cracked lug structures. For validation of the analytic stress intensity factors of cracked lugs, FEM with singular finite elements is used. Good agreement between computation and experimental results for fatigue life of aircraft cracked lugs was obtained. To determine crack trajectory of cracked structural components under mixed modes,, conventional singular finite elements and X-FEM are used.