Authors: Boljanović, Slobodanka 
Affiliations: Mechanics 
Mathematical Institute of the Serbian Academy of Sciences and Arts 
Title: Aircraft Lug Failure Design Under Fatigue Loading
Series/Report no.: Lecture Notes in Networks and Systems
Volume: 792 LNNS
First page: 294
Last page: 308
Related Publication(s): New Trends in Engineering Research : Proceedings of the International Conference of Experimental and Numerical Investigations and New Technologies, CNNTech 2023
Issue Date: 1-Jan-2024
ISBN: 978-3-031-46431-7
978-3-031-46432-4
ISSN: 2367-3370
DOI: 10.1007/978-3-031-46432-4_25
Abstract: 
For high speed systems, fatigue relevant analysis of lug-type joints plays an important role in preventing sudden hazard events. Dynamic loads are one of the main causes of system disturbance during service operations. In the present research, thus, the stress state of the lug with an elliptical corner crack-like flaw was explored, and prognostic analysis in terms of residual life was performed using a new computational framework. This study provides valuable information for both academia and industry on the detrimental effects of stress raisers for improving the optimal and safe design of fatigue-critical lug type joints.
Keywords: Computational design | Elliptical flaw | Fatigue life | Lug-Pin joint
Publisher: Springer Link

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