| 000 | 02073nam a2200241 a 4500 | ||
|---|---|---|---|
| 001 | vtls000040762 | ||
| 003 | KUKTEM | ||
| 005 | 20251114204419.0 | ||
| 008 | 090724t2008 my a f m 000 0 eng|d | ||
| 020 | _aTHE0005730(Local) | ||
| 039 | 9 |
_a201905221011 _bhanafiah _c201107132243 _dVLOAD _c200908141651 _dVLOAD _c200908141632 _dVLOAD _y200907240955 _zida84 |
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| 040 | _aUMP | ||
| 090 | _aTA417.7.T4 R64 2008 rs Bc. | ||
| 100 | 0 | _aRohani Daud | |
| 245 | 1 | 3 |
_aAn experimental strength of coach peel rivets joining similar and dissimilar sheet materials / _cRohani Daud |
| 246 | 3 |
_aAn experimental strength of coach peel rivets joining similar and dissimilar sheet materials _h[electronic resource] |
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| 260 |
_aKuantan, Pahang : _bUMP, _c2008 |
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| 300 |
_a45 p. : _bill. (some col.) ; _c30 cm. + _e1 computer disc |
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| 502 | _aProject paper (bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2008 | ||
| 520 | 3 | _aThe multi-materials structure has been applied as one of the methods in weight reduction especially in automotive industry. In this thesis, tensile test were performed in order to analyze the strength of similar and dissimilar sheet material joins connected rivets. It is used aluminum and steel sheet materials. Besides that, it is to study the fundamental phenomenon of tensile strength acted on coach peel riveted joints under similar and dissimilar sheet materials. Both materials are combined together to obtain the best comprise between weight reduction and the strength of the structure. The specimens of riveted joining was evaluated with tensile test in order to find the elastic of modulus (E), ultimate strength (σut), yield strength (σy), proportional limit (σpl) and the fracture point (εf) from stress-strain diagram. The tensile strength for similar specimens is 22.25 MPa. While for the dissimilar sheet materials is 22.20 MPa. The percentage of difference between both specimens is very small, 0.22%. | |
| 650 | 0 | _aRiveted joints | |
| 999 |
_aVIRTUA40 _c1617 _d1623 |
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| 999 | _aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5200*6500*9992 | ||