Progressive Damage Numerical Modelling and Simulation of Aircraft Composite Bolted Joints Bearing Response

Progressive Damage Numerical Modelling and Simulation of Aircraft Composite Bolted Joints Bearing Response

Finite element numerical progressive damage modelling and simulations applied to the strength prediction of airframe bolted joints on composite laminates can lead to shorter and more efficient product cycles in terms of design, analysis and certification, while benefiting the economic manufacturing...

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Bibliographic Details
Main Authors: Guoqiang Gao, Luling An, Ioannis K. Giannopoulos, Ning Han, Ende Ge, Geng Hu
Format: Article
Language:English
Published: MDPI AG 2020-12-01
Series:Materials
Subjects:
structural joints
mechanical testing
strength
numerical modelling
Online Access:https://www.mdpi.com/1996-1944/13/24/5606

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