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Table 1 Material properties and mesh type assigned to the FE model

From: Preliminary exploration of the biomechanical properties of three novel cervical porous fusion cages using a finite element study

Component

Element type

Material model

Material property

Cross-Sectional Area (mm2)

Cortical bone

C3D4

Isoelastic

E = 10000 MPa, v = 0.3

-

Cancellous bone

C3D4

Isoelastic

E = 100 MPa, v = 0.3

-

End plate

C3D8

Isoelastic

E = 5.6 MPa, v = 0.3

-

Facet cartilage

C3D4

Isoelastic

E = 10.4 MPa, v = 0.4

-

Nucleus pulpous

C3D8H

Hyperelastic

C10 = 0.12, C01 = 0.09

-

Annulus fibrosus matrix

C3D8H

Hyperelastic

C10 = 0.133, C01 = 0.0333, D = 0.6

-

Annulus fibers

T3D2

Hypoelastic

E = 350-550 MPa, v = 0.3

-

ALL

T3D2

Nonlinear

Force–deflection curvea

6.1

PLL

T3D2

Nonlinear

Force–deflection curvea

5.4

IL

T3D2

Nonlinear

Force–deflection curvea

13.1

CL

T3D2

Nonlinear

Force–deflection curvea

46.6

LF

T3D2

Nonlinear

Force–deflection curvea

50.1

Titanium alloy

C3D4

Isoelastic

E = 110000 MPa, v = 0.3

-

  1. ALL Anterior longitudinal ligament, PLL Posterior longitudinal ligament, IL Interspinous ligament, CL Capsular ligament, LF Ligamentum flavum, C3D4 Tetrahedron, C3D8 Hexahedron, C3D8H 8-node hybridization unit, T3D2 Truss, tension only. aLigament properties are referred to Fig. 2 for details