Fatigue threshold crack propagation in air and dry argon for a ti-6al-4v alloy RJ. Bucci, PC. Paris, RW. Hertzberg, RA. Schmidt, AF. Anderson

Format:

• Book

Author/Creator:

• Anderson, AF., author.
• Bucci, RJ., author.
• Hertzberg, RW., author.
• Paris, PC., author.
• Schmidt, RA., author.

Contributor:

• ASTM International
• American Society for Testing and Materials
• American Society for Testing and Materials.

Language:

English

Subjects (All):

• Fatigue--Congresses.
• Fatigue.
• Fracture mechanics--Congresses.
• Metals--Fracture--Congresses.
• Strains and stresses--Congresses.
• Strains and stresses.
• Argon.
• Crack propagation.
• Cracking (fracturing).
• Environmental tests.
• Fatigue (materials).
• Fatigue tests.
• Fractures (materials).
• Morphology.
• Stress ratio.
• Tension.
• Titanium alloys.

Physical Description:

1 online resource (16 pages) illustrations, figures, tables

Place of Publication:

West Conshohocken, Pa. ASTM International 1972

Summary:

Fatigue crack propagation experiments on a Ti-6A1-4V alloy were carried out within the framework of linear elastic fracture mechanics. Crack propagation results encompassing a wide range of fatigue crack growth rates, ?a/?N, and stress intensity range, ?K, were plotted in the conventional manner (that is, log-log plots of ?a/?N as a function of ?K) for studies conducted in room temperature air and dry argon environments. Corresponding fatigue striations formed in both environments were measured and compared with macroscopic crack extension rates

Notes:

• Includes bibliographical references
• Online resource; title from publisher's website, viewed December 19, 2016

Related Work:

American Society for Testing and Materials. Selected Technical Papers