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Session 4: Welding and Coating

The deformation and residual stress simulation of dual laser-beam bilateral synchronous welding for Al-alloy aircraft panel structure

Xiaohong Zhan, Nanjing University of Aeronautics and AstronauticsFollow
Yun Liu, Nanjing University of Aeronautics and AstronauticsFollow
Yao Meng, Nanjing University of Aeronautics and AstronauticsFollow
Wenmin Ou, Nanjing University of Aeronautics and AstronauticsFollow
Yanhong Wei, Nanjing University of Aeronautics and AstronauticsFollow

Presentation Type

Oral Presentation

Keywords

DLBSW, welding simulation, aluminum alloy, aircraft panel

The deformation and residual stress simulation of dual laser-beam bilateral synchronous welding for Al-alloy aircraft panel structure.docx (873 kB)

Included in

Aviation Commons, Structural Materials Commons

COinS

The deformation and residual stress simulation of dual laser-beam bilateral synchronous welding for Al-alloy aircraft panel structure