Crack incubation in shot peened AA7050 and mechanism for fatigue enhancement-Reference-Cited by-同舟云学术

Crack incubation in shot peened AA7050 and mechanism for fatigue enhancement

Published:2017-06-15 Issue:1 Volume:41 Page:71-83
ISSN:8756-758X
Container-title:Fatigue & Fracture of Engineering Materials & Structures
language:en
Short-container-title:Fatigue Fract Eng Mater Struct

Author:

Chadwick Daniel J.¹,Ghanbari Siavash²,Bahr David F.²,Sangid Michael D.¹²^ORCID

Affiliation:

1. School of Aeronautics and Astronautics Purdue University 701 W. Stadium Ave West Lafayette IN 47907‐2045 USA

2. School of Materials Engineering Purdue University 701 W. Stadium Ave West Lafayette IN 47907‐2045 USA

Funder

Office of Naval Research

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials,General Materials Science

Link

https://onlinelibrary.wiley.com/doi/pdf/10.1111/ffe.12652

Reference52 articles.

1. ElberW.The effects of shot peening residual stresses on the fracture and crack growth properties of D6AC steel. NASA Langley Research Centre Report No. TM X‐71943.1974.

2. Analysis of the effects of controlled shot peening on fatigue damage of high strength aluminium alloys

3. Optimisation of the fatigue resistance of 2024-T351 aluminium alloys by controlled shot peening—methodology, results and analysis

4. Bending fatigue behaviour of differently shot peened Al 6082 T5 alloy

5. An evaluation of shot peening, residual stress and stress relaxation on the fatigue life of AISI 4340 steel

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