Retardation effects due to overloads in aluminium-alloy aeronautical components-Reference-Cited by-同舟云学术

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Retardation effects due to overloads in aluminium-alloy aeronautical components

Published:2017-02-08 Issue:9 Volume:40 Page:1484-1500
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Engng Mater Struct

Author:

Maligno A. R.¹,Citarella R.²^ORCID,Silberschmidt V. V.³

Affiliation:

1. Institute for Innovation in Sustainable Engineering; University of Derby; Derby DE1 3HD UK

2. Department of Industrial Engineering; University of Salerno; Fisciano SA Italy

3. Wolfson School of Mechanical and Manufacturing Engineering; Loughborough University; Loughborough UK

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/ffe.12591/fullpdf

Reference24 articles.

1. Non-linear MSD crack growth by DBEM for a riveted aeronautic reinforcement;Citarella;Advances in Engineering Software,2009

2. FML full scale aeronautic panel under multiaxial fatigue: experimental test and DBEM simulation;Armentani;Engineering Fracture Mechanics,2011

3. MSD crack propagation on a repaired aeronautic panel by DBEM;Citarella;Advances in Engineering Software,2011

4. Multiple crack propagation by DBEM in a riveted butt-joint: a simplified two-dimensional approach;Citarella;Frattura ed Integrità Strutturale,2016

5. Residual strength evaluation by DBEM for a cracked lap joint;Citarella;Frattura ed Integrità Strutturale,2015

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1. Thoughts on the Importance of Similitude and Multi-Axial Loads When Assessing the Durability and Damage Tolerance of Adhesively-Bonded Doublers and Repairs;Aerospace;2023-11-07

2. Fatigue and creep-fatigue crack growth in aviation turbine disk simulation models under variable amplitude loading;Engineering Failure Analysis;2022-01

3. Code development for the computational analysis of crack propagation in structures;Frattura ed Integrità Strutturale;2020-05-19

4. The potential for structural simulation to augment full scale fatigue testing: A review;Progress in Aerospace Sciences;2020-02

5. Simulation of the delay effect after applying a simple overload on alloys of aluminum 2024T351 using the Willemborg model;Frattura ed Integrità Strutturale;2019-12-12

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