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AEM - FEM Comparison:
Obstacles Facing Finite Element Method (FEM): The main obstacle facing FEM when modeling structures is the modeling of large cracks and element separation. Although there are several FEM techniques that enable element separation, these are still limited to small problems with limited cracking and separation and cannot be generalized for use by practicing engineers in a full structural application. Using FEM, the element separation location can be either pre-defined by the user or automated; however, both solutions are impractical. Pre-defining the location controls the site of element separation, an event unknown in many cases, especially during structural collapse. Automation of element separation can be done using the Element Erosion Technique by removing damaged elements from the analysis when certain damage criteria are met. This also is not a practical solution as the crack width is limited to the element size and will cause cracks of large size that will never close in an application like earthquake loads. This solution will also not work when it comes to large scale problems when full structures are being modeled if we consider all of the elements to be close in size to the expected crack width.
Advantages in using the Applied Element Method (AEM): The main advantages of using AEM center around its ability to reliably and accurately predict structural behavior beginning with the initial loading stages, into crack initiation, through propagation on to complete collapse. AEM’s algorithms facilitate complex structural analysis without any user intervention and without artificial assumptions as to where or when cracks will occur.
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FEM
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AEM
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CPU Time
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Short
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Short
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D.O.F (Degrees of freedom)
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16 per element (8-node element)
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6 per element
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Cracking Model
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Smeared cracks and physical cracks (interface cracks, ones whose locations should be predefined)
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Smeared cracks and automatic physical cracks
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Joint elements (interface elements) are needed at the locations of wide cracks for simulating physical cracks.
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No need for joint elements
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Cracks cannot extend from element to element, making the structure inseparable at arbitrary locations
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Cracks propagates easily at element boundaries in any direction
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Location of joint elements (interface elements) should be predefined before analysis
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No need for joint elements
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Crack propagation cannot be followed accurately in smeared crack zones
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All crack propagation can be followed
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Preprocessing Time
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Long
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Short
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Reinforcement Details
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Very difficult to accurately account for reinforcement details as properties should be added at integration point locations
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All reinforcement details, for each reinforcement bar are accounted for. For example, bar area and concrete cover can be taken into account.
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Before Collapse
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High Accuracy
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High Accuracy
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During & After Collapse
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Can not follow collapse behavior
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High Accuracy
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