Crack path of in-service fatigued fan titanium disk of D-18T gas-turbine engine of the aircraft An-124-Reference-Cited by-同舟云学术

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Crack path of in-service fatigued fan titanium disk of D-18T gas-turbine engine of the aircraft An-124

Published:2022 Issue: Volume:39 Page:327-332
ISSN:2452-3216
Container-title:Procedia Structural Integrity
language:en
Short-container-title:Procedia Structural Integrity

Author:

Shanyavskiy Andrey,Soldatenkov Aleksey

Publisher

Elsevier BV

Subject

General Engineering,Energy Engineering and Power Technology

Reference17 articles.

1. Tumanov, A.T. (Ed.), 1975. Aircraft Materials, Handbook (in 9 vol.), 1975. VIAM, Moscow (in Russian).

2. Fracture of an Aircraft Horizontal Stabilizer;Howard,1986

3. Probabilistic Description of Fatigue Crack Growth in a Titanium Alloy Notched Member;Kocanda,2001

4. Failures in inspection procedures: case studies;McEvily;Eng. Fail. Anal.,2004

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1. Influence of crystallographic orientation on fatigue crack at notch of Inconel 718 alloy;Computational Materials Science;2024-03

2. A study on thermal behaviour of thermal barrier coating: investigation of particle size, YSZ/polysilazane, time and temperature curing effect;RSC Advances;2024

3. Crystal Plasticity-Driven Evaluation of Notch Fatigue Behavior in In718;2024

4. Crystal Plasticity-Driven Evaluation of Notch Fatigue Behavior in In718;2024

5. Fracture Toughness of Ti6Al4V/Cp-Ti Multi-Material Produced via Selective Laser Melting;Metals;2023-10-13

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