Effect of long-term stress and temperature exposure on the fracture toughness of Ti-62222 alloy

Engineering Fracture Mechanics

Volumn 64, Issue 6, 1999, Pages 799-803

  Singhal, Sameer ^a   Tucker, Jill ^a   Saxena, A ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

Aging; Creep; Fracture toughness; Titanium alloy

Indexed keywords

AGING OF MATERIALS; CRACKS; CREEP; FRACTURE TOUGHNESS; STRESS INTENSITY FACTORS; STRESSES; TENSILE STRENGTH; TENSILE TESTING; THERMAL EFFECTS; TITANIUM SHEET;

LONG-TERM STRESSES;

TITANIUM ALLOYS;

CREEP; FRACTURE MECHANICS; STRESS; TESTING;

EID: 0342980397     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0013-7944(99)00098-3     Document Type: Article

References (3)

1. Standard practice for R curve determination. In: ASTM E561. 1986 Annual book of ASTM standards. 3.01. American Society for Testing and Materials Philadelphia, PA, 1986. p. 615-634.
2. Lineberger, Lane. Titanium aerospace alloy. Advanced Materials and Processes. 153:(5):1998;45-46.
3. Norris R., Saxena A., Tucker J. Elevated temperature deformation and crack growth behavior in titanium alloy 6-2222. Engineering Fracture Mechanics. 62:1999;79-93.