Cold expansion effects on cracked fastener holes under constant amplitude and spectrum loading in the 2024-T351 aluminum alloy-Reference-Cited by-同舟云学术

Cold expansion effects on cracked fastener holes under constant amplitude and spectrum loading in the 2024-T351 aluminum alloy

Published:2014-11 Issue: Volume:68 Page:209-216
ISSN:0142-1123
Container-title:International Journal of Fatigue
language:en
Short-container-title:International Journal of Fatigue

Author:

Warner Jacob John,Clark Paul N.,Hoeppner David W.

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference17 articles.

1. Fatigue Technologies Inc., FTI process specification 8101D cold expansion of holes using the standard split sleeve system and countersink cold expansion (CsCx™), Seattle, WA, USA; 2002.

2. Phillips JL. Sleeve cold working fastener holes. Air Force Materials Laboratory AFML-TR-74-10. 1, D6–26271-6. Wright Patterson Air Force Base; 1974.

3. Air Force Structures, Structures Bulletin EN-SB-08-012, Revision B – Nondestructive inspection capability guidelines for United States Air Force aircraft structures, Wright-Patterson AFB, OH, USA; 2011.

4. American Society for Testing Materials (ASTM). Standard test method for measurement of fatigue crack growth rates (E 647). Am Soc Test Mater, West Conshohocken, PA., USA; 2000.

5. Fatigue Technologies Inc. (FTI), FTI process specification 8101D cold expansion of holes using the standard split sleeve system and countersink cold expansion (CsCx™), Seattle, WA, USA; 2002.

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