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    Numerical Simulation of Mechanical Effects in Composite Structures by the Finite Element Method

    Source: Journal of Pressure Vessel Technology:;2001:;volume( 123 ):;issue: 002::page 248
    Author:
    C. Müller
    ,
    A. Bohmann
    DOI: 10.1115/1.1319503
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In electromagnetic railgun experiments at ISL, the composite projectiles are accelerated up to 2000 m/s with a maximal acceleration of 7×106 m/s2. The maximum forces typically will have been achieved after 200 μs. One consequence of this dynamic load is a strain rate in the order of ε̇=2000 s−1, a rate at which metals are also giving up their static properties. The aim of research at ISL is the construction of a fiber-reinforced sabot adapted for dynamic bearing. FE simulations support the construction process as well as allowing a detailed study of the mechanical effects occurring during the acceleration of the sabot. The most important problem of dynamical simulation of composites is an adequate material model. We show in this paper, that the classical homogenized laminate models are insufficient to be used in dynamics. To develop an appropriate material model, we investigated selected materials statically as well as dynamically and we compared the experimental results with those of their numerical simulation. For a first material model approach, we made quasi-static experiments with a special sabot geometry. The quasi-static investigations have revealed that different conditions, e.g., lateral support, involve a completely different system answer. We found that a specimen without radial strain has more than the double strength of a specimen that allows radial strain, whereby the system answer still remains linear elastic and only very little internal delamination occurs. A second step toward a material model consists of dynamic experiments with specimens in a simple cylinder geometry on a Split Hopkinson Pressure Bar test facility. The specimens are made of fiber-reinforced epoxy, as well as metal-matrix composites. The dynamic experiments proved the strain as principal failure criterion for dynamic bearing, whereby the failure strain depends upon the momentary strain rate. Failure strain is also a historical function, so that the deformation history is important. We can show that the viscous polymer matrix plays a very important role for the dynamic toughness of reinforced materials. When the material fails, the stress is far beyond that of static failure: up to two times the static strength has been measured. Experiments with real sabots in railguns have shown that the failure occurs a relatively long time after the stress has achieved its maximum.
    keyword(s): Structures , Composite materials , Fibers , Computer simulation , Laminates , Force , Pressure , Finite element methods , Failure , Stress , Geometry , Projectiles , Toughness , Boundary-value problems , Deformation , Materials properties AND Epoxy adhesives ,
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      Numerical Simulation of Mechanical Effects in Composite Structures by the Finite Element Method

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    https://yetl.yabesh.ir/yetl1/handle/yetl/125762
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    • Journal of Pressure Vessel Technology

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    contributor authorC. Müller
    contributor authorA. Bohmann
    date accessioned2017-05-09T00:05:48Z
    date available2017-05-09T00:05:48Z
    date copyrightMay, 2001
    date issued2001
    identifier issn0094-9930
    identifier otherJPVTAS-28100#248_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/125762
    description abstractIn electromagnetic railgun experiments at ISL, the composite projectiles are accelerated up to 2000 m/s with a maximal acceleration of 7×106 m/s2. The maximum forces typically will have been achieved after 200 μs. One consequence of this dynamic load is a strain rate in the order of ε̇=2000 s−1, a rate at which metals are also giving up their static properties. The aim of research at ISL is the construction of a fiber-reinforced sabot adapted for dynamic bearing. FE simulations support the construction process as well as allowing a detailed study of the mechanical effects occurring during the acceleration of the sabot. The most important problem of dynamical simulation of composites is an adequate material model. We show in this paper, that the classical homogenized laminate models are insufficient to be used in dynamics. To develop an appropriate material model, we investigated selected materials statically as well as dynamically and we compared the experimental results with those of their numerical simulation. For a first material model approach, we made quasi-static experiments with a special sabot geometry. The quasi-static investigations have revealed that different conditions, e.g., lateral support, involve a completely different system answer. We found that a specimen without radial strain has more than the double strength of a specimen that allows radial strain, whereby the system answer still remains linear elastic and only very little internal delamination occurs. A second step toward a material model consists of dynamic experiments with specimens in a simple cylinder geometry on a Split Hopkinson Pressure Bar test facility. The specimens are made of fiber-reinforced epoxy, as well as metal-matrix composites. The dynamic experiments proved the strain as principal failure criterion for dynamic bearing, whereby the failure strain depends upon the momentary strain rate. Failure strain is also a historical function, so that the deformation history is important. We can show that the viscous polymer matrix plays a very important role for the dynamic toughness of reinforced materials. When the material fails, the stress is far beyond that of static failure: up to two times the static strength has been measured. Experiments with real sabots in railguns have shown that the failure occurs a relatively long time after the stress has achieved its maximum.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleNumerical Simulation of Mechanical Effects in Composite Structures by the Finite Element Method
    typeJournal Paper
    journal volume123
    journal issue2
    journal titleJournal of Pressure Vessel Technology
    identifier doi10.1115/1.1319503
    journal fristpage248
    journal lastpage252
    identifier eissn1528-8978
    keywordsStructures
    keywordsComposite materials
    keywordsFibers
    keywordsComputer simulation
    keywordsLaminates
    keywordsForce
    keywordsPressure
    keywordsFinite element methods
    keywordsFailure
    keywordsStress
    keywordsGeometry
    keywordsProjectiles
    keywordsToughness
    keywordsBoundary-value problems
    keywordsDeformation
    keywordsMaterials properties AND Epoxy adhesives
    treeJournal of Pressure Vessel Technology:;2001:;volume( 123 ):;issue: 002
    contenttypeFulltext
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