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PhD Fekete - SZIE version - 2.2 - Szent István Egyetem

PhD Fekete - SZIE version - 2.2 - Szent István Egyetem

PhD Fekete - SZIE version - 2.2 - Szent István Egyetem

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Literature review<br />

The presented model [Van Eijden et al., 1986] describes a set of non-linear equations<br />

(nine equations), which was solved by Newton-Raphson iteration process [Newton, 1711,<br />

Raphson, 1690]. The model can be applied primarily for static situations, and the transmission<br />

of the forces is realized by the followings: a force F q exerted by the quadriceps tendon is<br />

counteracted by a force F pt in the patellar tendon. The resultant force of these two forces is the<br />

F pf , the patellofemoral compression force, which is the reaction force between the patella and<br />

the femur.<br />

The most important findings of the authors are the followings:<br />

I. The authors found the relationship of the angle between the patellar tendon axis and the<br />

tibial axis (β) as a function of flexion angle (Figure <strong>2.2</strong>5).<br />

II.<br />

The authors found the relationship of the angle between the patellar tendon and the<br />

patellar axis (ρ) as a function of flexion angle (Figure <strong>2.2</strong>6).<br />

III. The authors found the relationship of the angle between the patellar axis and the femoral<br />

axis (ε) as a function of flexion angle (Figure <strong>2.2</strong>7).<br />

IV. The authors found the relationship of the angle between the quadriceps tendon and the<br />

femoral axis (ψ) as a function of flexion angle (Figure <strong>2.2</strong>8).<br />

V. The authors found the relationship of the angle between the quadriceps tendon and the<br />

patellar axis (ξ) as a function of flexion angle (Figure <strong>2.2</strong>9).<br />

VI. The authors provided the F pt /F q and F pf /F q ratios as a function of flexion angle<br />

(Figure 2.30 and Figure 2.31).<br />

The above-mentioned angles are represented on Figure <strong>2.2</strong>4.<br />

Figure <strong>2.2</strong>4. Anatomical angles<br />

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