The effects of prolonged thermal exposure on the mechanical properties and fracture toughness of C458 aluminum–lithium alloy

Author:

Ortiz D.,Brown J.,Abdelshehid M.,DeLeon P.,Dalton R.,Mendez L.,Soltero J.,Pereira M.,Hahn M.,Lee Eui,Ogren J.,Clark R.,Foyos J.,Es-Said O.S.

Publisher

Elsevier BV

Subject

General Engineering,General Materials Science

Reference7 articles.

1. Starke Jr EA, Blankenship Jr CP. In: Bhat BN, Bales TT, Vesely Jr EJ, editors. Aluminum–lithium alloys proceedings of aluminum–lithium alloys for aerospace applications workshop, May 17–19, NASA George C. Marshall Space Flight Center; 1994.

2. Venema GB, Rioja RJ. The manufacture of AFLC-458 plate at ALCOA Davenport Works and Lot Release Properties. In: Proceedings of aluminum–lithium workshop, Wright-Patterson AFB, Bass Lake Lodge, August 18; 1998.

3. Parrish C, Barba J, Min H, Peraza J, Foyos J, Lee EW, et al. Alternate heat treatments of C458 aluminum–lithium alloys, in aluminum alloys, their physical and mechanical properites. In: Proceedings of the 7th international conference ICAA7, Charlottesville, VA, April 9–14, 2000; Materials Science Forum, vols. 331–337; 2000. p. 655–62.

4. Characterization of cryogenic mechanical properties of aluminum–lithium alloy C-458;Vander Kooi;Scr Mater,1999

5. The effects of prolonged thermal exposure on the fracture and fatigue behavior of aluminum–lithium alloy 8090;Venkateswara Rao;Metall Trans A,1993

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