Engineering Journal: Science and InnovationELECTRONIC SCIENCE AND ENGINEERING PUBLICATION
Certificate of Registration Media number Эл #ФС77-53688 of 17 April 2013. ISSN 2308-6033. DOI 10.18698/2308-6033
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Article

Investigation of Fatigue Durability of Bolted Joints of Aircraft Structures in Numerical Simulation in the ANSYS Workbench Software Package

Published: 20.04.2026

Authors: Lyuminarskiy S.E., Alekseev A.D.

Published in issue: #4(172)/2026

DOI:

Category: Mechanics | Chapter: Mechanics of Deformable Solid Body

The article is devoted to numerical modeling of bolted joints of aircraft structures in order to assess their fatigue life under combined block-program loading. One of the key tasks in constructing mathematical models is the rational simplification of the geometry of parts without a noticeable deterioration in the accuracy of calculations. This is especially important for bolted joints, because modeling the threads on each bolt is a laborious process and requires a large amount of RAM. As a technique, finite element modeling of a bolted joint in ANSYS Workbench with a simplified representation of the thread is proposed. Five different variants of simulations, differing in geometry and type of contact, were investigated, and the results were compared with a reference model reproducing a full-fledged thread. A calculation model of the bolted connection has been established, which allows us to obtain the most optimal estimate of the calculated durability value. The proposed model has the lowest durability value, which provides an additional margin of safety during design.

EDN RAEYOO


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