Al-Li alloy 1441 for fuselage applications

Materials Science Forum

Volumn 331-337 II, Issue , 2000, Pages 907-912

  Bird, R K ^a   Dicus, D L ^a   Fridlyander, J N ^b   Sandler, V S ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b ALL RUSSIAN SCIENTIFIC RESEARCH INSTITUTE OF AVIATION MATERIALS   (Russian Federation)

Author keywords

Al Li; Fatigue Crack Growth; Fatigue Life; Fuselage Pressurization Fatigue; Tensile Properties; Toughness

Indexed keywords

COLD ROLLING; CRACK PROPAGATION; FATIGUE OF MATERIALS; FATIGUE TESTING; FRACTURE TOUGHNESS; FUSELAGES; STIFFNESS; TENSILE PROPERTIES;

FATIGUE CRACK GROWTH RATE; FUSELAGE PRESSURIZATION FATIGUE;

ALUMINUM ALLOYS;

EID: 0033875629     PISSN: 02555476     EISSN: None     Source Type: Book Series    
DOI: 10.4028/www.scientific.net/msf.331-337.907     Document Type: Article

References (5)

1. Altenpohl, Dietrich G.: Aluminum: Technology, Applications, and Environment, sixth edition. Aluminum Association, Inc., Washington, D.C. and the Minerals, Metals & Materials Society, Warrendale, Pennsylvania, 1998, pp. 340-342.
2. Graham, R.H.; Rioja, R.J.; and Newman, J.M.: "Al-Li Alloy Development". Aluminum-Lithium, Volume I, M. Peters and P.-J. Winkler, eds. Proceedings of the Sixth International Aluminum-Lithium Conference in Garmisch-Partenkirchen, FRG, 1991, pp. 15-24.
3. Fridlyander, J.N; Bratukhin, A.G.; and Davydov, V.G.: "Soviet Al-Li Alloys of Aerospace Application". Aluminum-Lithium, Volume I, M. Peters and P.-J. Winkler, eds. Proceedings of the Sixth International Aluminum-Lithium Conference in Garmisch-Partenkirchen, FRG, 1991, pp. 35-42.
4. Fridlyander, J.N; Bird, R.K.; Sadcov, V.V.; and Sandler, V.S.: "Al-Li (1441) High Technology and Service Life Alloy for Fuselage". Proceedings of the 5th International Symposium on Air Technologies for the 21st Century, August 8, 1999, Moscow, Russia.
5. Bird, R.K. and Dicus, D.L.: "Evaluation of Pressurization Fatigue Life of 1441 Al-Li Fuselage Panel". NASA Technical Memorandum TM-1999-209684, October 1999.