Fields of residual stresses near filled assemblage holes of the aircraft wing panel-Reference-Cited by-同舟云学术

Fields of residual stresses near filled assemblage holes of the aircraft wing panel

Published:2024-06-23 Issue:6 Volume:90 Page:59-75
ISSN:2588-0187
Container-title:Industrial laboratory. Diagnostics of materials
language:
Short-container-title:Zavod. lab., Diagn. mater.

Author:

Eleonsky S. I.¹,Zaitsev M. D.¹,Matvienko Yu. G.²,Pisarev V. S.¹

Affiliation:

1. N. E. Zhukovsky Central AeroHydrodynamics Institute

2. Mechanical Engineering Research Institute of the Russian Academy of Science

Publisher

TEST-ZL Publishing

Reference20 articles.

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2. Belov V. K., Kaliuta A. A., Rudzey G. F. The provision of fatigue durability of aircraft structures by technology means. — Novosibirsk: Izd. NGTU, 2012. — 404 p. [in Russian].

3. Furukawa A., Kamiya K., Hagiwara M. Effect of the Residual Stress on the Fatigue Strength of a Bolt in Bolt/Nut Assemblies (Verification of the hypotheses using an axi-symmetric bolt model) / Journal of Advanced Mechanical Design, Systems, and Manufacturing. 2012. Vol. 6. N 1. P. 189 – 197.

4. Yunbo Bi, Jiefeng Jiang, Yinglin Ke. Effect of interference fit size on local stress in single lap bolted joints / Advances in Mechanical Engineering. 2015. Vol. 7. N 6. P. 1 – 12. DOI: 10.1177/1687814015590307

5. Keith W. J., Ralph W. B. Investigation of residual stress relaxation in cold expanded holes by the slitting method / Engineering Fracture Mechanics. 2017. Vol. 179. P. 213 – 224. DOI: 10.1016/j.engfracmech.2017.05.004