Applied Element Method (AEM)

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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.

 

FEM

AEM

CPU Time

Short

Short

D.O.F (Degrees of freedom)

16 per element (8-node element)

6 per element

Cracking Model

Smeared cracks and physical cracks (interface cracks, ones whose locations should be predefined)

Smeared cracks and automatic physical cracks

Joint elements (interface elements) are needed at the locations of wide cracks for simulating physical cracks.

No need for joint elements

Cracks cannot extend from element to element, making the structure inseparable at arbitrary locations

Cracks propagates easily at element boundaries in any direction

Location of joint elements (interface elements) should be predefined before analysis

No need for joint elements

Crack propagation cannot be followed accurately in smeared crack zones

All crack propagation can be followed

Preprocessing Time

Long

Short

Reinforcement Details

Very difficult to accurately account for reinforcement details as properties should be added at integration point locations

All reinforcement details, for each reinforcement bar are accounted for. For example, bar area and concrete cover can be taken into account.

Before Collapse

High Accuracy

High Accuracy

During & After Collapse

Can not follow collapse behavior

High Accuracy


 
A comparison of AEM vs. FEM

 

 

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