scholarly journals Knee Arthroplasty Bone Model with Double Layer Array Synthesis and Evaluation of Finite Element Analysis

2012 ◽  
Vol 16 (3) ◽  
pp. 189-194
Author(s):  
Ismail Hakki Korkmaz ◽  
Irfan Kaymaz ◽  
Fatih Medetalibeyolu ◽  
Omer Selim Yildirim
2013 ◽  
Vol 32 (2) ◽  
pp. 338-345 ◽  
Author(s):  
Oh-Ryong Kwon ◽  
Kyoung-Tak Kang ◽  
Juhyun Son ◽  
Sae-Kwang Kwon ◽  
Seung-Bae Jo ◽  
...  

Author(s):  
Eric Rohrs ◽  
Manish Paliwal ◽  
D. Gordon Allan

Aseptic loosening of the tibial implant is one of the major reasons of failure in Total Knee Arthroplasty (TKA). The cement viscosity at the time of application to the bone influences the cement penetration and stability of the prosthesis. Four cements of different viscosities and set times were selected for analysis (Simplex-P, DePuy-2, Palacos, and Endurance). Finite element analysis was used to model cement flow and cement mantle resulting from a surgically implanted tibial plate into sawbone open cell blocks simulating tibial cancellous bone (Pacific Research, WA). Frictional stress, pressure, sliding distance, and total stress at the bone-cement-stem interface were studied at the contact interfaces, which may contribute towards construct stability. Palacos had the maximum interface pressure, sliding distance, and total stress, while DePuy-2 displayed the lowest total stress and sliding distance at interface. Simulated flow profile correlated well with the cemented constructs’ radiographic profiles.


2008 ◽  
Vol 41 ◽  
pp. S237 ◽  
Author(s):  
Daniel Kluess ◽  
Christine Schultze ◽  
Anja Lubomierski ◽  
Wolfram Mittelmeier ◽  
Klaus-Peter Schmitz ◽  
...  

2013 ◽  
Vol 389 ◽  
pp. 1065-1068
Author(s):  
Li Tang ◽  
Jing Tao Yue ◽  
Yin Zhang

According to the design criteria referred to CCAR-25,the static strengths of accessorial equipments (single stretcher-supporting equipment, double layer stretcher-supporting equipment and nursing-type unit) and the track-mounting mechanism applied to fix the accessorial equipments to the seat tracks of the airliner are analyzed under five loads by using the software MSC.PATRAN. Based on the analysis results, the strengths of the accessorial equipments will be checked, the structures can satisfy the requirements of strength.


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