2015
DOI: 10.1051/smdo/2015008
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Failure mechanism of PMI foam core sandwich beam in bending

Abstract: -Polymethacrylimide (PMI) foams have been widely applied in aerospace engineering as the core material of sandwich structures. This paper proposes a modified model to predict the constitutive relation of PMI foams and compares it to existing testing data. The study is then applied to the investigation of the failure mechanism of PMI foam core sandwich beams in bending. Corresponding bending tests were carried out where a complex failure process was observed through a high-speed camera. Numerical model of the f… Show more

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Cited by 11 publications
(9 citation statements)
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“…However, the indentation failure mode does not lead to the final failure of the sandwich beam. More specifically, the core material experiences flexure and shear stress during the static loading . As the indenter moves further down, the shear stress gradually increases.…”
Section: Resultsmentioning
confidence: 99%
See 1 more Smart Citation
“…However, the indentation failure mode does not lead to the final failure of the sandwich beam. More specifically, the core material experiences flexure and shear stress during the static loading . As the indenter moves further down, the shear stress gradually increases.…”
Section: Resultsmentioning
confidence: 99%
“…PMI foam could be simulated using the low-density foam model in Abaqus, a pseudo hyperelastic formulation, and its failure mechanics incorporated the maximum principal stress criterion. 31 As the compression and shear modes dominated the core deformation during the bending process, the current study required as input the stress–strain response of the foam for the uniaxial compression and tensile test. The Poisson’s ratio of the foam was assumed to be zero, implying that the evaluation of the stress–strain response became uncoupled along the principal deformation directions.…”
Section: Finite Element Modelingmentioning
confidence: 99%
“…Many studies in the field of sandwich structures have been conducted to assess the performance of their mechanical properties, both with and without simulations, and to understand the complex interactions between different composite materials. Moreover, several studies have demonstrated the behavior and failure modes of composite sandwich structures under bending load by considering the following factors: reinforcement materials [ 1 , 2 , 3 ], skin stacking sequences [ 4 ], foam types [ 5 , 6 , 7 , 8 , 9 , 10 , 11 ], adhesive types, and manufacturing conditions. Regarding high-performance applications, composite sandwich structures have been used in aeronautical materials [ 12 ], sailboat hulls [ 2 , 5 ], wind turbine blades [ 11 , 13 , 14 ], marine applications [ 15 ], and aerospace engineering [ 16 , 17 , 18 ].…”
Section: Introductionmentioning
confidence: 99%
“…4,52,54 -56 Many works are devoted to obtaining and studying the characteristics of sandwich materials and products obtained using PMI. 8,57 -62 All these issues require separate consideration and are not the subject of this review.…”
Section: Introductionmentioning
confidence: 99%