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خانه / بایگانی برچسب: abaqus johnson cook damage

بایگانی برچسب: abaqus johnson cook damage

Simulation SPH explosion over the composite panel( Aluminum- Metal Foam) in Abaqus-Damage investigation

In this tutorial, the Simulation SPH explosion over the composite panel( Aluminum- Metal Foam) in Abaqus-Damage investigation – has been done. The explosive part, or the TNT is modeled as a three-dimensional solid part. The aluminum sheets are modeled as three-dimensional solid parts. The Aluminum Foam as a core is ...

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Simulation CEL explosion in the depth of soil near a solid steel pipe in Abaqus

In this tutorial, the Simulation CEL explosion in the depth of soil near a solid steel pipe in Abaqus  has been done. The Eulerian domain is modeled as a three-dimensional Eulerial part. The air, soil, and TNT are modeled as three-dimensional solid part. The steel pipe is model as a ...

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Simulation drilling hole process in concrete by using a rigid drill tool in Abaqus

In this tutorial, the Simulation drilling hole process in the Abaqus by using a rigid drill tool has been studied.  Concrete drilling, or core drilling, is the process of drilling precise holes in concrete floors or walls, or in any other paved surfaces or structures. The concrete is modeled as a three-dimensional solid part. ...

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Numerical simulation of three-point bending of the composite panel(ceramic-Steel-Aluminum) in Abaqus

In this tutorial, Numerical simulation of three-point bending of the composite panel(ceramic-Steel-Aluminum) in Abaqus has been investigated. The ceramic and steel plates are modeled as a three-dimensional solid part. The aluminum core with honeycomb shape is modeled as a three-dimensional shell part. Three rigid bodies are used to define hydraulic ...

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Simulation low-velocity impact response and damage mechanism of glass fiber aluminium laminates in Abaqus

In this tutorial Simulation low-velocity impact response and damage mechanism of glass fiber aluminium laminates in Abaqus has been studied.Glass fiber aluminium laminate (GLARE) is a kind of fiber metal laminates widely applied in aircraft structures, frequently subjected to low-velocity impact incidents. The purpose of this paper is to investigate ...

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