Fracture assessment of laser beam welded aluminium panels

11th International Conference on Fracture 2005, ICF11

Volumn 8, Issue , 2005, Pages 6184-6189

  Seib, E ^a   Kocak M ^a   Assler, H ^b   Pacchione, M ^b  

^a INSTITUTE OF MATERIALS RESEARCH   (Germany)

^b AIRBUS OPERATIONS GMBH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AL-ALLOY; ALUMINIUM PANELS; EXPERIMENTAL VALUES; FAILURE LOAD; FRACTURE ASSESSMENT; SMALL SCALE; STRUCTURAL INTEGRITY ASSESSMENT PROCEDURES; TENSILE LOADS; THIN-WALLED; WELD MATERIAL; WELD STRENGTH; WELDED PANELS;

AEROSPACE APPLICATIONS; ALUMINUM; FRACTURE; LASER BEAMS; STRENGTH OF MATERIALS; WELDS;

WELDING;

EID: 84869751292     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. SINTAP: Structural integrity assessment procedure for European industry. Final procedure. Brite Euram Project No. BE95-1426, British Steel, 1999
2. K.-H. Schwalbe. Introduction of δ5 as an operational definition of the CTOD and its practical use. Fracture Mechanics: 26th volume, ASTM STP 1256, 1995
3. H. Tada, P. C. Paris, and G. R. Irwin. The stress analysis of cracks handbook. New York: ASME Press, 3rd edition, 2000
4. K.-H. Schwalbe, Y.-J. Kim, S. Hao, A. Cornec, and M. Koçak. EFAM ETM-MM 96: The ETM method for assessing the significance of crack-like defects in joints with mechanical heterogeneity (strength mismatch). GKSS Report 97/E/9, GKSS Research Center, 1997
5. E. Seib, M. Koçak, H. Assler. Fracture assessment of welded aerospace Al-alloys using SINTAP route. DVM-Bericht 236, Feb. 17-18, 2004 in Cologne/Germany.