Finite element method simulation of shotpeening wing skin panel
(Beijing Aeronautical Manufacturing Technology Research Institute, Beijing , China)
Abstract: Finite element method(FEM) was used to simulate the forming process of shotpeening the wing skin panel. Experiment of shotpeeing the wing skin panel was carried out. The results show that equivalent deformation in shotpeening process can be obtained using the elongation and bending result caused by thermal stress that is induced by applying temperature load on the surface of the part. Deformation of the part in the shotpeeing process can be analyzed using this method. The parameters and their relationships are identified.
Key words: wing skin panel; shotpeen forming; simulation; finite element method