The in‐service fatigue fracture mechanisms for the I‐stage low‐pressure compressor disk of the aircraft engine D30KU‐154-Reference-Cited by-同舟云学术

The in‐service fatigue fracture mechanisms for the I‐stage low‐pressure compressor disk of the aircraft engine D30KU‐154

Published:2022-10-25 Issue:2 Volume:46 Page:728-741
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Eng Mat Struct

Author:

Shanyavskiy Andrey¹²^ORCID,Nikitin Ilia¹,Nikitin Alexander¹

Affiliation:

1. Institute for Computer Aided Design of the Russian Academy of Sciences Moscow Russia

2. Aviation Register of the Russian Federation Moscow Russia

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.13868

Reference35 articles.

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3. ShanyavskiyAA.Modeling of Metal Fatigue fracture.Monographia Ufa;2007:498.

4. Failures in inspection procedures: case studies

5. KrasnowskiBR ReddyDJ FranadaBG ReidL RestisJ.Fatigue strength and damage tolerance of thin‐walled riveted structures with cold‐worked holes.American Helicopter Society 56th Annual Forum Florida;2000: 1383‐1394.

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