Adams Advanced Package > FE Part > Appendix > FE Part Compared to Other Methods for Geometric Nonlinearity

FE Part Compared to Other Methods for Geometric Nonlinearity

The FE Part modeling object is accurate for beam-like structures undergoing very large deformation; that is, geometric nonlinearity. Therefore one will want to compare this approach with other common approaches for modeling geometrically nonlinear flexibility of beam-like structures in Adams. The other principal approaches are:
Discrete Flexible Link: a series of rigid bodies connected by Adams Solver BEAM, FIELD or BUSHING force objects
Multi MNF: a series of modal neutral file (MNF) based Adams Flex linear flexible bodies connected by fixed joint type constraints or bushings
There are advantages (pros) and disadvantages (cons) of each approach:
FE Part
Pros
Geometrically nonlinear and distributed mass formulation does not require subdivision in lumped masses or linear flexible components
Modification and parameterization is often easier than the other two approaches
Modeling a distributed load via the FE Load is far less time consuming than using discrete force vectors or MFORCES
Support for stress and strain recovery in APostProcessor (X-Y plots)
Reduced noise in nonlinear contact where a geometry "wraps" around another since the geometry is not discretized
No "seams" in the stress/strain results due to discretization
Refining or coarsening the model (number of nodes in this case) is often easier than in the other two approaches
2D formulation option for faster analysis on planar problems
Cons
No support for AControls
No support for Adams2Nastran export
No support for stress and strain recovery in APostProcessor (animated color contour plots)
Discrete Flexible Link
Pros
Can be defined in a preloaded/pre-stressed condition (and support model save/reload)
Support for ALinear
Full support for AControls
Supports use of 2D parts for faster analysis on planar problems
Cons
Time consuming to modify and parameterize (Adams command language skill required in many instances)
Time consuming to apply distributed loads to it
No direct support for stress/strain recovery (need to write your own requests)
Refining or coarsening the discretization is somewhat time consuming without Adams command language skill
Mass properties approximated by discretization
Multi MNF
Pros
Can be defined in a preloaded/pre-stressed condition (and support model save/reload)
Support for ALinear
Full support for AControls
Modal stress/strain recovery (X-Y plots and animated color contour plots)
Distributed mass properties
Cons
Model setup is time consuming (MNF generation for discretization of what is usually a single piece of geometry)
Higher skill required for model setup (definition of interaction between discrete flexible bodies is not straightforward to do correctly)
Time consuming to modify and parameterize aspects of it requiring MNF re-generation (shape, material and so on.)
Sometimes time consuming to work with applied distributed loads (MFORCE workflow)
Refining or coarsening the discretization is time consuming
No 2D option
Another consideration is model solve time. On this consideration it is difficult to compare the three approaches generally speaking. The comparisons are expected to be model dependent. One would want to compare the coarsest model which achieves sufficiently accurate results from the various approaches. Model coarseness/fineness is defined by number of nodes (FE Part), parts (discrete flexible link) or flexible bodies (multi-MNF).