| 000 | 02042nam a2200265 a 4500 | ||
|---|---|---|---|
| 001 | vtls000052455 | ||
| 003 | KUKTEM | ||
| 005 | 20251114204444.0 | ||
| 008 | 110329t2010 my a f m 000 0 eng d | ||
| 020 | _aTHE0005622(Local) | ||
| 039 | 9 |
_a201905171143 _bhanafiah _c201107140042 _dVLOAD _y201103291455 _zida |
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| 040 | _aUMP | ||
| 090 | _aTA347.F5 N45 2010 rs Bc. | ||
| 100 | 1 | _aNg, Kok Chuan | |
| 245 | 1 | 0 |
_aDevelopment of impact strength model for human synthetic bone / _cNg Kok Chuan |
| 246 | 3 |
_aDevelopment of impact strength model for human synthetic bone _h[electronic resource] |
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| 260 |
_aKuantan, Pahang : _bUMP, _c2010 |
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| 300 |
_axv, 54 p. : _bill. (some col.) ; _c30 cm. + _e1 computer discs |
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| 502 | _aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2010 | ||
| 504 | _aBibliography : p. 52 | ||
| 520 | 3 | _aDue to current demand, the usage of synthetic bone had increased dramatically during these recent years. The main purpose of this project is to develop and analyze the impact strength model for human synthetic bone. The impact test simulation was done in finite element analysis (FEA). The bone model geometry will be designed in Solidwork environment and imported into finite element environment for FEA Finite element analysis will be carried out in MSC. Patran/Marc and Algor respectively. Major input data to FEM were isotropic material model, solid element type (tetrahedral in MSC. Marc and brick in Algor), constraints and impact load. Material properties were taken from literature. The model were validated with published experimental results. Predicted stress-strain response of synthetic bone was agreeable with published report. Based on the analysis results, MSC. Marc model is better than Algor. The result obtained shows the response of synthetic bone towards impact loading. | |
| 650 | 0 |
_aBones _xMechanical properties |
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| 650 | 0 | _aFinite element methods | |
| 999 |
_aVIRTUA40 _c2319 _d2325 |
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| 999 | _aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992 | ||