Responses of damage and energy of sandwich and multilayer beams composed of metallic face sheets and aluminum foam core under bending loading

被引:10
|
作者
Sha, J. B. [1 ]
Yip, T. H.
Sun, Jun
机构
[1] Bei Hang Univ, Sch Mat Sci & Engn, Beijing 100083, Peoples R China
[2] Nanyang Technol Univ, Sch Mat Engn, Singapore 639698, Singapore
[3] Xian Jiaotong Univ, Sch Mat Sci & Engn, Key State Lab Mech Behav Mat, Xian 710049, Peoples R China
关键词
D O I
10.1007/BF02586216
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This present article deals with bending deformation and failure behavior of sandwich and multilayer beams composed of aluminum foam core and metallic face sheets analyzed by in-situ surface displacement analysis (SDA). The effect of beam structure on the failure mode of beam and the energy absorbed by beam failure were investigated and discussed. The SDA results revealed that collapse of the sandwich beams is by two basic modes, indentation (ID) and core shear (CS). The ID is localized deformation on the beam adjacent to the inner or outer roller in four-point bending, where displacement and compressive strains are at the maximum. As for CS mode, failure occurs in the core between inner and outer rollers, which corresponds to the maximum shear strain; discontinuous displacements in both the vertical and horizontal directions are the primary factors for shear crack initiation, growth, and broadening. The failure of the multilayer beams depends on whether the face sheets show ID mode or otherwise. If a single layer core sandwich fails in ID mode, the multilayer beams with similar face sheets show mixed ID + CS modes. If a single layer core sandwich fails fully in CS mode, no ID characteristic appears in the similar face sheet multilayer beams. The deformation energy of the beams relates strongly to the structure and geometry of beam. The predication of the bending fracture work W, of a beam is given by W-x/W-5 = 0.3875 C + 0.9383 where W-5 is the deformation energy of the beam with a 5-mm core, and C is the thickness ratio of the core x to 5 mm.
引用
收藏
页码:2419 / 2433
页数:15
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