On the fatigue and fracture behavior of necked double shear lugs for aircraft applications-Reference-Cited by-同舟云学术

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On the fatigue and fracture behavior of necked double shear lugs for aircraft applications

Published:2020-03 Issue:3 Volume:51 Page:284-296
ISSN:0933-5137
Container-title:Materialwissenschaft und Werkstofftechnik
language:en
Short-container-title:Materialwiss. Werkstofftech.

Author:

Winklberger M.¹,Schagerl M.¹

Affiliation:

1. Johannes Kepler University Linz, Institute of Structural Lightweight Design Altenberger Str. 69 4040 LINZ AUSTRIA

Funder

Austrian Research Promotion Agency

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics,General Materials Science

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1002/mawe.201900220

Reference23 articles.

1. FATIGUE CRACK GROWTH IN LUGS

2. S.E. Larsson Fatigue Design Procedures 4thICAF Symposium. Pergamon Press 1969.

3. J. Schijve Contributions to the theory of aircraft structures Delft University Press Nijgh-Wolters-Noordhoff University Publishers Rotterdam 1972.

4. W.T. Kirkby D.P. Rooke Fracture mechanics in engineering practice Applied Scientific Publications London 1977.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Crack size monitoring in necked double shear lugs using the electro-mechanical impedance method;Health Monitoring of Structural and Biological Systems XV;2021-03-22

2. Crack Identification in Necked Double Shear Lugs by Means of the Electro-Mechanical Impedance Method;Sensors;2020-12-23

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