Creep age forming of 2024A, 8090 and 7449 alloys

Materials Science Forum

Volumn 331, Issue , 2000, Pages

  Pitcher, P D ^a   Styles, C M ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY LABORATORY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AGING OF MATERIALS; AIRCRAFT MATERIALS; FORMABILITY; METAL FORMING; PLASTIC DEFORMATION; RESIDUAL STRESSES; STRESS RELAXATION; TENSILE STRENGTH;

AIRCRAFT STRUCTURES; CREEP AGE FORMING; DAMAGE TOLERANCE; SPRINGBACK;

ALUMINUM ALLOYS;

EID: 0033884675     PISSN: 02555476     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (5)

1. M.C. Holman, J. Mechanical Working Technology 20 (1989), p. 477.
2. A. Levers, Proc. ABAQUS World Users Conf., Newport Rhode Is., (1998).
3. th Conf on Aluminium-Lithium Alloys, DGM, (1992), p. 1371.
4. Airbus Industrie Material Specification, Aluminium Alloy 7449-T7951, AIMS 03-02-016, (1998).
5. M. Peters, V. Bachmann and K. Welpmann, Al-Li Alloys, TMS-AIME, Warrendale, (1981), p. 293.