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CHAPTER 9Element Formulations

Linear Strain Triangle (LST) Elements

Physical Intuition: Moving Beyond Constant Strain

In our journey through two-dimensional (2D) finite element formulations, the Constant Strain Triangle (CST) served as the gateway to plane elasticity. While the CST—a three-node, linear-displacement triangular element—is conceptually simple and computationally cheap, it exhibits severe physical and mathematical limitations. Specifically, because the displacement field within a CST is linear, the resulting strain and stress fields are spatially constant. In any real-world structural component, stress is rarely uniform; it concentrates, peaks, and decays in response to geometric features (such as holes, fillets, notches, or crack tips) and localized boundary conditions.

To approximate these rapid changes—known as stress concentration gradients—using CST elements, an analyst must refine the mesh to an extreme degree. Even then, the constant-stress approximation results in a jagged, discontinuous representation of stress across element boundaries, which converges slowly and demands massive computational resources. Furthermore, CST elements suffer from shear locking (or parasitic shear) when subjected to bending, artificially stiffening the structure because a linear displacement field cannot represent the curved, parabolic shear strain profiles of flexural deformation.

To resolve these shortcomings, we introduce the Linear Strain Triangle (LST) element. The LST is a quadratic, higher-order triangular element. By adding three midside nodes along the edges of the triangle, we increase the total number of nodes from three to six. This structural upgrade allows us to interpolate displacements quadratically rather than linearly.

Mathematically, the quadratic displacement field produces a linear strain field (and consequently, a linear stress field) within the element. This allows a single LST element to represent linear variations in strain and stress, making it exceptionally proficient at capturing steep stress gradients and bending behaviors with a fraction of the mesh density required by CST elements.

LST 6-NODE QUADRATIC TRIANGLE 1 (0, 0) 4 (a/2, 0) 2 (a, 0) 5 (a/2, b/2) 3 (0, b) 6 (0, b/2)

Core Concepts

1. Higher-Order Elements and Pascal's Triangle

The choice of interpolation polynomial determines the kinematic capability of a finite element. For two-dimensional elements, we can visualize the polynomial terms using Pascal's Triangle:

$$\begin{array}{ccccccccc} & & & & 1 & & & & \\ & & & x & & y & & & \\ & & x^2 & & xy & & y^2 & & \\ & x^3 & & x^2y & & xy^2 & & y^3 & \\ x^4 & & x^3y & & x^2y^2 & & xy^3 & & y^4 \end{array}$$

Linear Triangle (CST): Uses the first three terms ($1, x, y$). This requires 3 nodes (one at each vertex) to solve for the 3 unknown coefficients of the polynomial.
Quadratic Triangle (LST): Uses the first six terms ($1, x, y, x^2, xy, y^2$). This complete quadratic polynomial requires 6 nodes to determine its 6 coefficients.

The completeness of the quadratic polynomial is crucial. Because it contains all terms up to the second degree ($x^2, xy, y^2$), the element possesses geometric isotropy (or spatial invariance). This means the element shows no bias toward any coordinate direction, and its physical behavior is independent of the coordinate system's orientation.

If we were to drop any of the quadratic terms (e.g., using a 4-node or 5-node triangle), the element would lose coordinate invariance, violating basic physical principles.

2. The Role of Midside Nodes

Midside nodes are positioned at the midpoints of the element boundaries. They serve two vital functions:

Kinematics: They double the degrees of freedom (DOFs) per element from 6 (in CST) to 12 (in LST). Each node has two translational DOFs ($u_i, v_i$). The extra DOFs provide the mathematical degrees of freedom necessary to interpolate the displacement field quadratically.
Geometric Mapping (Isoparametric Curved Boundaries): By using quadratic shape functions to map the coordinates, the boundaries of the LST element do not have to be straight lines; they can be curved quadratic parabolas. This allows the LST element to conform perfectly to curved boundaries, such as circular holes, cylindrical fillets, or pressure vessels, without requiring an infinite number of straight segments.

3. Continuous vs. Discontinuous Stress Fields ($C^0$ vs. $C^{-1}$)

In displacement-based FEM, we enforce compatibility (continuity of displacements) across element boundaries. For both CST and LST elements, the displacement field is continuous across shared edges, which represents $C^0$ continuity.

However, because strain and stress are obtained by taking derivatives of the displacement field:

In CST elements, the first derivative of a linear displacement is a constant. The strain is constant within each element, leading to step-change discontinuities (a $C^{-1}$ field) at element boundaries.
In LST elements, the first derivative of a quadratic displacement is a linear function. The strain and stress vary linearly within the element. While they are still discontinuous at element boundaries, the linear variation allows the stress field to smoothly trace steep gradients, resulting in much smaller stress jumps and vastly improved stress recovery.

4. Area Coordinates (Natural Coordinates)

Integrating functions over arbitrary triangular shapes in Cartesian coordinates $(x,y)$ is mathematically tedious because the limits of integration are coupled. To simplify the mathematical formulations and integrations, we use Area Coordinates (also called natural or triangular coordinates), denoted by $L_1, L_2,$ and $L_3$.

Consider a triangle with vertices 1, 2, and 3. Any point $P$ inside the triangle divides it into three sub-triangles: $\Delta_1$ (opposite Node 1, formed by $P$, 2, and 3), $\Delta_2$ (opposite Node 2, formed by $P$, 3, and 1), and $\Delta_3$ (opposite Node 3, formed by $P$, 1, and 2).

LST SUB-AREAS PARTITIONED BY POINT P Node 1 Node 2 Node 3 P Δ₂ Δ₁ Δ₃

We define the area coordinates as the ratio of these sub-areas to the total area $A$:

$$L_1 = \frac{A_1}{A}, \quad L_2 = \frac{A_2}{A}, \quad L_3 = \frac{A_3}{A}$$

Area coordinates possess several unique properties:

1.
Partition of Unity: Since the sum of the sub-areas equals the total area ($A_1 + A_2 + A_3 = A$), the sum of the coordinates must be unity:
$$L_1 + L_2 + L_3 = 1$$

This relationship implies that only two of the three area coordinates are independent. If we know $L_1$ and $L_2$, then $L_3 = 1 - L_1 - L_2$.

2.
Kronecker Delta at Vertices: At vertex 1, the point $P$ coincides with Node 1, meaning $A_1 = A$ and $A_2 = A_3 = 0$. Thus:
$$(L_1, L_2, L_3) = (1, 0, 0) \quad \text{at Node 1}$$

Similarly:

$$(L_1, L_2, L_3) = (0, 1, 0) \quad \text{at Node 2}$$
$$(L_1, L_2, L_3) = (0, 0, 1) \quad \text{at Node 3}$$
3.
Linearity on Edges: Along the edge opposite Node $i$, the coordinate $L_i = 0$. For instance, on the line connecting Node 2 and Node 3, $L_1 = 0$. At the midpoint of edge 1-2, the coordinates are $(0.5, 0.5, 0)$.

5. Comparison: CST vs. LST

To appreciate the advancement of the LST formulation, let us compare the two elements:

PropertyConstant Strain Triangle (CST)Linear Strain Triangle (LST)
:---:---:---
Nodes3 (vertices only)6 (3 vertices + 3 midside nodes)
Degrees of Freedom6 (2 per node)12 (2 per node)
Displacement fieldLinear ($u = a_0 + a_1 x + a_2 y$)Quadratic ($u = a_0 + a_1 x + a_2 y + a_3 x^2 + a_4 xy + a_5 y^2$)
Strain / Stress fieldSpatially constantSpatially linear
Shear LockingSusceptible (requires very fine mesh)Highly resistant
Boundary FittingStraight edges onlyCurved (parabolic) edges possible
Displacement Convergence$O(h^2)$$O(h^3)$
Stress Convergence$O(h)$$O(h^2)$

Extended chapter reference

Quadratic triangular interpolation, midside nodes, curved boundaries, and stress gradients

The six-node LST enriches the triangular displacement field with quadratic terms. Its linear strain field captures bending and smooth gradients far more efficiently than the three-node CST.

Construct quadratic area-coordinate shape functions.
Map midside nodes and curved boundaries isoparametrically.
Integrate the spatially varying stiffness with suitable quadrature.
Compare h-refinement and p-enrichment for stress accuracy.

Visual map

From formulation to verified result

Linear Strain Triangle (LST) Elements finite element workflowA six-stage engineering workflow from model definition through verification.Linear Strain Triangle (LST) ElementsModel-to-evidence sequence1
Six-node geometry
2
Quadratic N
3
Jacobian mapping
4
Variable B matrix
5
Gauss integration
6
Gradient recovery
Each stage produces evidence for the next. A reliable result preserves traceability from the physical idealization to the final engineering check.

Equation sheet

Governing relationships

Vertex shape
$$N_1=L_1(2L_1-1)$$

Quadratic shape at a corner node.

Midside shape
$$N_4=4L_1L_2$$

Controls the edge between nodes 1 and 2.

Isoparametric map
$$x=\sum_{i=1}^{6}N_ix_i,\quad y=\sum_{i=1}^{6}N_iy_i$$

Uses the same interpolation for geometry and displacement.

Engineering comparison

Selection and interpretation table

PropertyCST / T3LST / T6Engineering effect
DisplacementLinearQuadraticImproved bending response
StrainConstantLinearCaptures gradients per element
Edge geometryStraightCan be curvedFits fillets more accurately
IntegrationOne point often exactMultiple points requiredHigher computational cost

Verification and application

Checks before accepting the result

  • Midside node order is correct
  • Jacobian stays positive
  • Curved edges follow geometry
  • Quadrature integrates the chosen material law

Industry application

For a pressure-vessel nozzle intersection, quadratic triangles fit curved boundaries and resolve the through-surface stress gradient with fewer elements than CST meshes, provided midside nodes are not severely distorted.