| Literature DB >> 24786914 |
R Mootanah1, C W Imhauser, F Reisse, D Carpanen, R W Walker, M F Koff, M W Lenhoff, S R Rozbruch, A T Fragomen, Z Dewan, Y M Kirane, K Cheah, J K Dowell, H J Hillstrom.
Abstract
A three-dimensional (3D) knee joint computational model was developed and validated to predict knee joint contact forces and pressures for different degrees of malalignment. A 3D computational knee model was created from high-resolution radiological images to emulate passive sagittal rotation (full-extension to 65°-flexion) and weight acceptance. A cadaveric knee mounted on a six-degree-of-freedom robot was subjected to matching boundary and loading conditions. A ligament-tuning process minimised kinematic differences between the robotically loaded cadaver specimen and the finite element (FE) model. The model was validated by measured intra-articular force and pressure measurements. Percent full scale error between FE-predicted and in vitro-measured values in the medial and lateral compartments were 6.67% and 5.94%, respectively, for normalised peak pressure values, and 7.56% and 4.48%, respectively, for normalised force values. The knee model can accurately predict normalised intra-articular pressure and forces for different loading conditions and could be further developed for subject-specific surgical planning.Entities:
Keywords: in vitro cadaveric test; knee joint contact mechanics; lower limb malalignment; model validation; osteoarthritis; subject-specific finite element knee model
Mesh:
Year: 2014 PMID: 24786914 PMCID: PMC4047624 DOI: 10.1080/10255842.2014.899588
Source DB: PubMed Journal: Comput Methods Biomech Biomed Engin ISSN: 1025-5842 Impact factor: 1.763
Figure 1.MRI images of the frontal view of the knee joint in (a) CUBE sequence for representation of meniscus and ligament and (b) SPGR sequence for representation of cartilage and bone.
Figure 2.3D LiveWire algorithm used to create geometries of the different tissues.
Figure 3.The use of the ‘non-manifold algorithm’ to create common contact areas between adjacent tissue, such as the distal femur and femoral cartilage. (a) The inner geometry of the cartilage was overestimated to protrude into the femur and eliminate any gap at the femur-cartliage boundary. (b) The non-manifold assembly technique superimposed the accurately identified femur with the overestimated cartilage image to remove overlaps between the femur and cartilage, creating a common boundary between the adjacent femur and cartilage surfaces.
Figure 4.3D solid geometry of the knee joint assembly created in CATIA CAD package.
Figure 5.Model preparation for hexagonal meshing. (a) A 3D spline was created near the edge of the cartilage surface. (b) The 3D spline was used to truncate the very thin edge to produce a finite thickness that would accommodate hexahedral elements.
Mesh sensitivity analysis on element size.
| Number of elements (element size) | ||||
|---|---|---|---|---|
| Femoral cartilage | Tibial cartilage | Menisci | Change in maximum contact pressure (%) | |
| Reference | 29,547 (0.75 mm) | 36,026 (0.5 mm) | 38,034 (0.5 mm) | – |
| Case 1 | 29,547 (0.75 mm) | 36,026 (0.5 mm) | 4314 (1mm) | 2.92 |
| Case 2 | 29,547 (0.75 mm) | 4988 (1mm) | 4314 (1mm) | 3.63 |
| Case 3 | 11,044 (1 mm) | 4988 (1mm) | 4314 (1mm) | 4.56 |
| Case 4 | 2558 (1.5 mm) | 1994 (1.5 mm) | 1224 (1.5 mm) | 15.68 |
| Case 5 | 1455 (2 mm) | 674 (2 mm) | 936 (2 mm) | 20.5 |
Note: Case 3 is 95% accurate compared with the reference case.
Mesh sensitivity analysis on element types (4-noded and 10-noded tetrahedral elements) for bone meshing.
| Force(N) | Contact pressure (MPa) | |||
|---|---|---|---|---|
| Lateral | Medial | Lateral | Medial | |
| RMSE (4-noded vs 10-noded tetrahedral elements) | 3.4372 | 9.02428 | 0.02763 | 0.05916 |
| Maximum value | 237.515 | 631.984 | 2.22 | 3.9 |
| %FSE | 1.4% | 1.4% | 1.2% | 1.5% |
Note: There was a maximum of 1.5% full-scale error (FSE) in force and contact pressure between the two element types.
Figure 6.(a) Boundary and loading conditions on the FE knee joint model: tied contact pair between (1) cartilage–bone, (2) ligament–bone and (3) tibia–fibula; contact pairs between (4) cartilage–meniscus and (5) cartilage–cartilage. The proximal femur was fixed in 6 degrees of freedom. A 374-N axial load was applied along the tibia, and varus/valgus bending moments, ranging from 0 to 15 Nm, were applied about the knee joint centre. (b) Anterior and (c) posterior views and of the knee joint FE model, displaying the hexagonal and tetrahedral mesh elements for the soft tissues and bones, respectively.
Figure 7.(a) Taylor Spatial Frame fixed to cadaveric leg for subsequent simulations of lower limb malalignments and corrections by HTO; (b) cadaveric knee, mounted on a 6-degree-of-freedom robot for controlled loading; (c) TekScan IScan sensor equilibration before calibration; (d) sensors fixed in vitro to the cruciate ligaments between the tibial cartilage and the femur; (e) pressure distribution in the knee joint during in vitro loading.
Figure 8.The ligament tuning process: the ligament properties were adjusted in an iterative process until the kinematics of the tibia relative to the femur in the model closely matched those in vitro in all six degrees of freedom for (a) translational and (b) rotational kinematics during a sagittal rotation from full extension to 65° flexion, and (c) translational and (d) rotational kinematics during a 374-N axial load and a 0–15-Nm valgus/varus bending moment.
Material properties assigned to the different tissues comprising the knee joint.
| Components | Modulus (MPa) | Poisson's ratio |
|---|---|---|
| Bone | Young's: 1000 | 0.3 |
| Cartilage | Young's: 25 | 0.45 |
| Meniscus | Circumferential E1: 120 | Out-of-plane: |
| Axial and radial: E2, E3: 20 | In-plane (circumferential) | |
| Shear G12, G13: 57.7 | ||
| Shear G23: 8.33 |
Source: (Perie and Hobatho 1998; Schreppers et al. 1990; Shepherd and Seedhom 1997; Shepherd and Seedhom 1999; Weiss and Gardiner 2001).
Figure 9.Material properties for the LCL, MCL, ACL and PCL at every angle of flexion, following the ligament tuning process.
Young's modulus values of the MCL, LCL, ACL and PCL before and after application of varus and valgus bending moments.
| Young's modulus(MPa) | ||||
|---|---|---|---|---|
| Bending moment | MCL | LCL | ACL | PCL |
| 15 Nm varus | 10 | 60 | 250 | 40 |
| ONm | 43 | 56 | 154 | 40 |
| 15 Nm valgus | 60 | 5 | 150 | 40 |
Note: Linear increments in ligament Young's moduli were applied in the model as bending moments increased from 0 to 15 Nm varus and 15 Nm valgus.
Figure 10.Evaluation of FE model. Pressure distributions in the tibio-femoral joint in response to a 374-N axial load and a 15-Nm varus/valgus bending moment for (a) in vitro testing and (b) FE model predictions. A, anterior; P, posterior; L, lateral; M, medial.
Figure 11.In vitro and FE-predicted medial and lateral compartment loading in response to a 374-N axial load and 0–15 Nm varus and valgus bending moments for (a) normalised peak pressure and (b) normalised force.
RMSE and percentage FSE in medial and lateral force and peak pressure values between in vitro and FE results for axial load of 374 N and varus/valgus bending moments ranging from 0 to 15 Nm.
| Medial compartment | Lateral compartment | Medial compartment | Lateral compartment | Force ratio | ||||||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Absolute force (N) | Normalised force | Absolute force (N) | Normalised force | Absolute pressure (MPa) | Normalised pressure | Absolute pressure (MPa) | Normalied pressure | Medial compartment | Lateral compartment | |||||||||||
| Bending moment (Nm) | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE | Exp | FE |
| 15 | 267 | 494 | 1.00 | 1.00 | 0 | 0 | 0 | 0 | 2.26 | 2.21 | 1 | 1 | 0 | 0 | 0 | 0 | 100 | 100 | 0 | 0 |
| 14 | 257 | 474 | 0.96 | 0.96 | 0 | 0 | 0 | 0 | 2.14 | 2.03 | 0.95 | 0.92 | 0 | 0 | 0 | 0 | 100 | 100 | 0 | 0 |
| 13 | 246 | 451 | 0.92 | 0.91 | 0 | 0 | 0 | 0 | 1.92 | 1.8 | 0.85 | 0.81 | 0 | 0 | 0 | 0 | 100 | 100 | 0 | 0 |
| 12 | 223 | 432 | 0.84 | 0.87 | 0 | 3 | 0 | 0.01 | 1.67 | 1.62 | 0.74 | 0.73 | 0 | 0 | 0 | 0 | 100 | 99 | 0 | 1 |
| 11 | 207 | 414 | 0.78 | 0.84 | 0 | 8 | 0 | 0.02 | 1.48 | 1.42 | 0.65 | 0.64 | 0 | 0 | 0 | 0 | 100 | 98 | 0 | 2 |
| 10 | 185 | 392 | 0.69 | 0.79 | 0 | 18 | 0 | 0.04 | 1.45 | 1.21 | 0.64 | 0.55 | 0 | 0 | 0 | 0 | 100 | 96 | 0 | 4 |
| 9 | 181 | 375 | 0.68 | 0.76 | 6 | 29 | 0.02 | 0.07 | 1.42 | 1.13 | 0.63 | 0.51 | 0.09 | 0.07 | 0.02 | 0.04 | 97 | 93 | 3 | 7 |
| 8 | 172 | 357 | 0.64 | 0.72 | 13 | 43 | 0.04 | 0.1 | 1.38 | 1.08 | 0.61 | 0.49 | 0.17 | 0.15 | 0.04 | 0.08 | 93 | 89 | 7 | 11 |
| 7 | 155 | 339 | 0.58 | 0.69 | 18 | 59 | 0.06 | 0.14 | 1.34 | 1.13 | 0.59 | 0.51 | 0.22 | 0.24 | 0.05 | 0.12 | 90 | 85 | 10 | 15 |
| 6 | 142 | 320 | 0.53 | 0.65 | 31 | 76 | 0.1 | 0.17 | 1.25 | 0.98 | 0.55 | 0.44 | 0.34 | 0.33 | 0.07 | 0.17 | 82 | 81 | 18 | 19 |
| 5 | 132 | 303 | 0.49 | 0.61 | 48 | 92 | 0.16 | 0.21 | 1.16 | 0.94 | 0.51 | 0.43 | 0.51 | 0.4 | 0.11 | 0.21 | 73 | 77 | 27 | 23 |
| 4 | 123 | 286 | 0.46 | 0.58 | 65 | 108 | 0.21 | 0.25 | 1.06 | 0.89 | 0.47 | 0.4 | 0.7 | 0.47 | 0.15 | 0.24 | 65 | 73 | 35 | 27 |
| 3 | 113 | 270 | 0.42 | 0.55 | 83 | 125 | 0.27 | 0.29 | 0.96 | 0.86 | 0.42 | 0.39 | 0.9 | 0.54 | 0.19 | 0.28 | 58 | 68 | 42 | 32 |
| 2 | 104 | 252 | 0.39 | 0.51 | 100 | 141 | 0.33 | 0.32 | 0.85 | 0.8 | 0.38 | 0.36 | 1.1 | 0.61 | 0.23 | 0.31 | 51 | 64 | 49 | 36 |
| 1 | 96 | 233 | 0.36 | 0.47 | 117 | 159 | 0.38 | 0.36 | 0.75 | 0.75 | 0.33 | 0.34 | 1.3 | 0.69 | 0.27 | 0.35 | 45 | 59 | 55 | 41 |
| 0 | 95 | 215 | 0.36 | 0.44 | 128 | 177 | 0.42 | 0.41 | 0.7 | 0.7 | 0.31 | 0.32 | 1.5 | 0.8 | 0.32 | 0.41 | 43 | 55 | 57 | 45 |
| − 1 | 90 | 190 | 0.34 | 0.38 | 147 | 203 | 0.48 | 0.47 | 0.59 | 0.62 | 0.26 | 0.28 | 1.8 | 0.95 | 0.38 | 0.49 | 38 | 48 | 62 | 52 |
| − 2 | 89 | 178 | 0.33 | 0.36 | 150 | 217 | 0.49 | 0.5 | 0.57 | 0.59 | 0.25 | 0.27 | 1.94 | 1.03 | 0.41 | 0.53 | 37 | 45 | 63 | 55 |
| − 3 | 86 | 166 | 0.32 | 0.34 | 154 | 228 | 0.5 | 0.52 | 0.56 | 0.55 | 0.25 | 0.25 | 2.1 | 1.06 | 0.44 | 0.54 | 36 | 42 | 64 | 58 |
| − 4 | 57 | 140 | 0.21 | 0.28 | 194 | 253 | 0.64 | 0.58 | 0.5 | 0.45 | 0.22 | 0.2 | 2.72 | 1.17 | 0.57 | 0.6 | 23 | 36 | 77 | 64 |
| − 5 | 52 | 124 | 0.19 | 0.25 | 202 | 270 | 0.66 | 0.62 | 0.49 | 0.37 | 0.22 | 0.17 | 2.93 | 1.25 | 0.62 | 0.64 | 20 | 31 | 80 | 69 |
| − 6 | 48 | 109 | 0.18 | 0.22 | 210 | 285 | 0.69 | 0.65 | 0.47 | 0.31 | 0.21 | 0.14 | 3.12 | 1.31 | 0.66 | 0.67 | 19 | 28 | 81 | 72 |
| − 7 | 27 | 94 | 0.1 | 0.19 | 243 | 300 | 0.8 | 0.69 | 0.39 | 0.21 | 0.17 | 0.1 | 3.54 | 1.37 | 0.75 | 0.7 | 10 | 24 | 90 | 76 |
| − 8 | 20 | 74 | 0.07 | 0.15 | 247 | 321 | 0.81 | 0.74 | 0.37 | 0.07 | 0.16 | 0.03 | 3.66 | 1.45 | 0.77 | 0.74 | 7 | 19 | 93 | 81 |
| − 9 | 10 | 54 | 0.04 | 0.11 | 255 | 340 | 0.84 | 0.78 | 0.33 | 0 | 0.15 | 0 | 3.8 | 1.53 | 0.8 | 0.78 | 4 | 14 | 96 | 86 |
| − 10 | 4 | 45 | 0.01 | 0.09 | 270 | 355 | 0.89 | 0.81 | 0.24 | 0 | 0.11 | 0 | 4.03 | 1.6 | 0.85 | 0.82 | 1 | 11 | 99 | 89 |
| − 11 | 0 | 34 | 0 | 0.07 | 278 | 373 | 0.91 | 0.86 | 0.1 | 0 | 0.04 | 0 | 4.2 | 1.68 | 0.88 | 0.86 | 0 | 8 | 100 | 92 |
| − 12 | 0 | 25 | 0 | 0.05 | 282 | 390 | 0.92 | 0.89 | 0 | 0 | 0 | 0 | 4.35 | 1.74 | 0.92 | 0.89 | 0 | 6 | 100 | 94 |
| − 13 | 0 | 20 | 0 | 0.04 | 296 | 401 | 0.97 | 0.92 | 0 | 0 | 0 | 0 | 4.52 | 1.8 | 0.95 | 0.92 | 0 | 5 | 100 | 95 |
| − 14 | 0 | 11 | 0 | 0.02 | 300 | 426 | 0.98 | 0.98 | 0 | 0 | 0 | 0 | 4.6 | 1.94 | 0.97 | 0.99 | 0 | 3 | 100 | 97 |
| − 15 | 0 | 8 | 0 | 0.02 | 305 | 436 | 1 | 1 | 0 | 0 | 0 | 0 | 4.75 | 1.95 | 1 | 1 | 0 | 2 | 100 | 98 |
| RMSE | 138.71 | 65.18 | 0.16 | 1.49 | 8.05 | 8.05 | ||||||||||||||
| FSE (%) | 28.08 | 7.56 | 14.59 | 4.48 | 0.07 | 6.67 | 0.31 | 5.04 | ||||||||||||
Note: Percentage FSE was obtained by expressing the RMSE as a percentage of the maximum corresponding value.
Figure 12.In vitro and FE-predicted forces in the medial and lateral compartments as a percentage of the total axial force during 0–15 Nm varus and valgus bending moments.
Figure 13.Static equilibrium diagrams showing forces and bending moment acting on the knee joint during (a) varus and (b) valgus lift off. FMCL = internal force in the MCL; FMCL = internal force in the LCL; M = bending moment.
Previously published validated or verified computational knee models.
| Authors and date | Parameters validated | Type of specimen |
|---|---|---|
| Kinematics of a multibody knee model | Identically loaded cadaveric knee | |
| Kinematics of three subject-specific FE total knee replacement models | ||
| Kinematics of the knee soft tissue FE model | ||
| Kinematics of an FE knee model | ||
| Kinematics of an FE knee model | Previously published experimental kinematic data | |
| Kinematics of an FE knee model | Previously published experimental kinematic data | |
| Kinematics of an FE knee model | Previously published experimental kinematic data | |
| Strain and displacement of an FE femur model | ||
| Kinematics of an FE knee model | ||
| Strain in tibia and femur of an FE knee model with a unilateral knee replacement (UKR) | ||
| Total load, peak load and peak load location for axial, varus and valgus loading conditions of a 2D discrete element analysis model | ||
| Knee joint stresses and strains – musculoskeletal multibody dynamics | Experimental findings from other investigators | |
| Joint contact pressures of an FE knee model | ||
| Joint contact pressures of an FE knee model | Experimental findings from other investigators |