Aluminum Alloy 7075 Ratcheting and Plastic Shakedown Evaluation with the Multiplicative Armstrong

Aluminum Alloy 7075 Ratcheting and Plastic Shakedown Evaluation with the Multiplicative Armstrong–Frederick Model

Published:2017-07 Issue:7 Volume:55 Page:2461-2470
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Agius Dylan¹,Kourousis Kyriakos I.²,Wallbrink Chris³,Hu Weiping³,Wang Chun H.⁴,Dafalias Yannis F.⁵

Affiliation:

1. RMIT University, Melbourne, Victoria 3001, Australia

2. University of Limerick, Limerick, V94 T9PX, Ireland

3. Defense Science and Technology Group, Melbourne, Victoria 3207, Australia

4. University of New South Wales, Sydney, New South Wales 2052, Australia

5. University of California, Davis, Davis, California 95616

Funder

Defence Science and Technology Organisation

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.J055833

Reference46 articles.

1. Fatigue Life Analysis of Specimens Subjected to Infrequent Severe Loading Using a Nonlinear Kinematic Hardening Cyclic Plasticity Model

2. Effect of mean stress and ratcheting strain on fatigue life of steel

3. An Investigation of Cyclic Transient Behavior and Implications on Fatigue Life Estimates

4. Effects of Strain Hardening on Response of Skin Panels in Hypersonic Flow

5. ArmstrongP. J.FrederickC. O. “A Mathematical Representation of the Multiaxial Bauschinger Effect,” Berkeley Nuclear Lab. Rept. RD/B/N 731, Berkeley, CA, 1966.

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