Six-Node Triangular Element (TRIA6)

Category: Structural Analysis | Integrated 2026-04-06
CAE visualization for tria6 element theory - technical simulation diagram
Six-Node Triangular Element (TRIA6)

Six-Node Triangular Element (TRIA6): Theoretical Foundations

LST Element โ€” The Superior Version of CST

๐Ÿง‘โ€๐ŸŽ“

Does the 6-node triangular element (TRIA6, LST) solve the problems of CST?


๐ŸŽ“

Yes. The LST (Linear Strain Triangle) is a quadratic triangular element where strain varies linearly within the element. It completely eliminates the constant strain problem of CST.


Shape Function

๐ŸŽ“

TRIA6 has three vertex nodes and three mid-side nodes. The shape functions are quadratic polynomials of the area coordinates $L_1, L_2, L_3$:


Vertex nodes:

$$ N_i = L_i(2L_i - 1) $$

Mid-side nodes:

$$ N_{ij} = 4L_i L_j $$

๐Ÿง‘โ€๐ŸŽ“

It's the 2D version of TET10, right?


๐ŸŽ“

Exactly. TRIA6 = 2D version of TET10, CST = 2D version of TET4. It's the same relationship.


Accuracy

  • Displacement: $O(h^3)$ (CST is $O(h^2)$)
  • Stress: $O(h^2)$ (CST is $O(h)$)

๐Ÿง‘โ€๐ŸŽ“

Same convergence rate as Q8, right?


๐ŸŽ“

Yes. Since TRIA6 and Q8 are elements of the same order (quadratic), they have the same convergence rate. However, Q8 has slightly higher accuracy per element (8-term vs. 6-term polynomial).


TRIA6 vs. Q8

CharacteristicTRIA6Q8
Automatic MeshingEasySomewhat Difficult
Accuracy per DOF70-80% of Q8Baseline
Curved Edge HandlingHas mid-side nodesHas mid-side nodes
Sensitivity to Mesh QualityMore robust than Q8Sensitive to distortion
Adaptive MeshingEasySomewhat Difficult
๐Ÿง‘โ€๐ŸŽ“

TRIA6 is inferior to Q8 in accuracy efficiency but superior in ease of mesh generation. It's the same pattern as TET10 vs. HEX20, right?


๐ŸŽ“

Perfect understanding. The pattern "triangles/tetrahedra are easy for automatic meshing, quadrilaterals/hexahedra have higher accuracy" is common in both 2D and 3D.


Numerical Integration

IntegrationPointsAccuracy
3-point Gauss (Full Integration)3Integrates quadratic polynomials exactly
1-point Gauss1Insufficient accuracy (not used)
7-point Gauss7Used for higher-order integration
๐Ÿง‘โ€๐ŸŽ“

Usually, 3 points are sufficient, right?


๐ŸŽ“

Yes. 3-point full integration is standard for TRIA6. Shear locking does not occur (because it's a quadratic element). Volume locking is also usually not a problem. It's a very stable element.


Summary

๐Ÿง‘โ€๐ŸŽ“

Let me organize the theory of TRIA6.


๐ŸŽ“

Key Points:


  • Quadratic Triangular Element (LST) โ€” Superior version of CST. Strain varies linearly.
  • 2D Version of TET10 โ€” Inherits the advantage of automatic meshing.
  • Same Convergence Rate as Q8 โ€” However, Q8 has higher DOF efficiency.
  • Robust to Mesh Quality โ€” More stable than Q8 even with distorted shapes.
  • 3-point Gauss Integration is Sufficient โ€” No locking.

๐Ÿง‘โ€๐ŸŽ“

If CST is the "do not use" element, then TRIA6 is the "use with confidence" element, right?


๐ŸŽ“

Exactly. TRIA6 is the most reliable triangular element for 2D automatic mesh analysis.


Coffee Break Trivia

TRIA6's Complete Quadratic Polynomial and Accuracy

The 6-node triangular element (TRIA6) has three vertex nodes and three mid-side nodes, using a complete quadratic polynomial (6 terms) for its shape functions. In area coordinates, the vertex shape functions are Li(2Li-1), and the mid-side ones are 4LiLj. At three times the computational cost of TRIA3 (linear), the stress error convergence rate for bending problems improves from h-squared to h-cubed. Records indicate that Browning, Abrahamson, and others first practically applied quadratic triangular elements to aircraft wing stress analysis in the late 1960s.

Computational Methods for the Six-Node Triangular Element (TRIA6)

TRIA6 Implementation

๐Ÿง‘โ€๐ŸŽ“

Please tell me the implementation considerations for TRIA6.


๐ŸŽ“

TRIA6 is more complex than CST but can be implemented standardly using numerical integration (3-point Gauss).


Element Names by Solver

VariationNastranAbaqusAnsys
StandardCTRIA6CPS6 (Plane Stress)PLANE183 (degenerated)
Plane StrainCTRIA6 + PLPLANECPE6PLANE183(degenerated,PE)
AxisymmetricCTRIAX6CAX6PLANE183(degenerated,Axi)
๐Ÿง‘โ€๐ŸŽ“

In Ansys, is TRIA6 not a dedicated element but a degenerated form of PLANE183?


๐ŸŽ“

Ansys's PLANE183 is an 8-node quadrilateral but is used degenerated into a 6-node triangle by placing mid-side nodes on three edges. However, internally, the correct TRIA6 formulation is used, not a degenerated CST.


Handling of Mid-Side Nodes

๐ŸŽ“

Similar to Q8/TET10, CAD curve snapping for mid-side nodes is important for TRIA6. It improves the approximation accuracy of curved boundaries.


๐ŸŽ“

Points to note:

  • Mid-side nodes should be within 25% to 75% of the edge length.
  • The Jacobian must be positive.
  • Use finer mesh in areas with high curvature.

TRIA6 Mesh Quality

MetricIdeal ValueAcceptable Range
Aspect Ratio1.0< 5.0
Minimum Angle60ยฐ> 20ยฐ
JacobianPositiveMust be positive
๐Ÿง‘โ€๐ŸŽ“

Are the quality requirements more lenient than for CST?


๐ŸŽ“

TRIA6 is more robust to element shape distortion than CST. The quadratic shape functions partially absorb distortion. However, accuracy degrades with extreme distortion like minimum angles below 10ยฐ.


Summary

๐Ÿง‘โ€๐ŸŽ“

Let me organize the numerical methods for TRIA6.


๐ŸŽ“

Key Points:


  • 3-point Gauss Integration is Standard โ€” Full integration, no locking.
  • CAD Snapping for Mid-Side Nodes โ€” Same caution as Q8, TET10.
  • Robust to Shape Distortion โ€” More stable than CST.
  • Dramatic Accuracy Improvement from CSTโ†’TRIA6 Conversion โ€” Effect of linearโ†’quadratic.

Coffee Break Trivia

3-Point Gauss Integration for TRIA6

TRIA6 typically uses 3-point or 7-point Gauss integration. The integration points for the 3-point scheme are placed at equal distances from the triangle's centroid (e.g., L1=L2=1/6, L3=2/3) and can integrate polynomials up to 5th order exactly. The 7-point scheme is a high-precision version proposed by Strang-Fix (1973), capable of fully integrating polynomials up to 7th order. Since the 3-point integration points become superconvergence points for stress sampling, the Zienkiewicz-Zhu method, which extrapolates stresses from these points to obtain nodal stresses, is widely used.

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