Fatigue Crack Growth Rate Measurements in Aluminum Alloy Forgings: Effects of Residual Stress and Grain Flow

Author:

Bush RW,Bucci RJ,Magnusen PE,Kuhlman GW

Publisher

ASTM International

Cited by 6 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. An Update on the Impact of Forging Residual Stress in Airframe Component Design;Materials Performance and Characterization;2018-04-01

2. The Impact of Forging Residual Stress on Fatigue in Aluminum;56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2015-01-02

3. A Case Study on the Application of ICME in Aircraft Design;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23

4. Reducing Residual Stress in 7050 Aluminum Alloy Die Forgings by Heat Treatment;Journal of Engineering Materials and Technology;2008-05-22

5. An integrated methodology for separating closure and residual stress effects from fatigue crack growth rate data;Fatigue & Fracture of Engineering Materials and Structures;2007-03

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