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The following four-article series serves as a comprehensive introduction to the analysis discipline known as the finite element method (FEM). Originally based on works by engineering consultant Steve Roensch, this guide has been updated to reflect modern simulation workflows.
Second in a four-part series.
Previous: Part 1: Introduction to FEA
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The Pre-processing Phase
As discussed in the introduction, finite element analysis is comprised of pre-processing, solution, and post-processing phases. The goals of pre-processing are to transform a "perfect" CAD model into a mathematical model by developing a mesh, assigning material properties, and applying realistic boundary conditions.
Meshing: Nodes and Elements
The finite element mesh subdivides the geometry into elements, which are connected at specific points called nodes. The solver calculates the primary variables (like displacement) at these nodes and interpolates the values across the elements.
Figure 1: The discretization process transforms continuous geometry into a mesh of nodes and elements for calculation.
- 2D / Thin Shell: For sheet metal or thin-walled structures, elements are effectively 2D (Triangles or Quads) but are "warped" to fit 3D space. This requires creating a "mid-surface" from the solid CAD geometry.
- 3D Solid: For bulky parts (castings, forgings), elements have thickness in all dimensions. Common types include the Hexahedral (Brick) and the Tetrahedral (Tet).
- Special Elements: Beams, springs, and masses are used to simplify models where full geometry isn't necessary.
Degrees of Freedom (DOF)
The "unknowns" that the solver must calculate are the Degrees of Freedom (DOF) at each node.
- Solid Elements: Typically have 3 DOF per node (Translations X, Y, Z). They do not carry rotational information directly.
- Shell/Beam Elements: Typically have 6 DOF per node (3 Translations + 3 Rotations). This allows them to calculate bending moments efficiently without modeling the physical thickness.
Preparing CAD for Analysis (Defeaturing)
Developing the mesh is often the most time-consuming task. Modern FEA integrates directly with CAD geometry, but raw manufacturing CAD is rarely ready for simulation.
Defeaturing is the process of removing cosmetic details (small fillets, engraved text, tiny holes) that create unnecessary complexity. A tiny fillet might force the mesher to create thousands of microscopic elements, skyrocketing computation time for zero accuracy gain.
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Meshing Strategies: Hex vs. Tet
The geometry is meshed using either a mapping algorithm or a free-meshing algorithm.
- Mapped Meshing (Hex/Brick): Creating a structured grid of brick elements. This is the "gold standard" for accuracy and efficiency but is difficult to apply to organic, complex shapes.
- Free Meshing (Tet): Automatically filling the volume with pyramids/tetrahedrons. While historically less accurate, modern Parabolic (2nd Order) Tetrahedral elements are highly accurate and are the industry standard for complex geometry because they can mesh almost any shape automatically.
Tip: Always check for element distortion (Aspect Ratio or Jacobian checks) before solving. A highly distorted element can cause mathematical errors or singularities.
Material Properties and Boundary Conditions
Materials: A linear static analysis requires, at minimum, the Elastic Modulus (Stiffness), Poisson's Ratio, and Density. Thermal analyses add Conductivity and Expansion Coefficients.
Boundary Conditions (BCs):
- Restraints (Fixtures): How is the part held? (e.g., Fixed Geometry, Hinge, Roller). Incorrect fixtures are the #1 cause of bad FEA data.
- Loads: Forces, Pressures, Gravity, or Thermal loads.
Best Practice: Always apply BCs to the geometry faces/edges rather than selecting individual nodes. This allows the FEA software to automatically update the load distribution if you remesh the part later.
Continue to Part 3:
Finite Element Analysis (FEA): The Solution Phase »
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