000 02195nam a2200253 a 4500
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003 KUKTEM
005 20251114204428.0
008 100603t2009 my dao f m 000 0 eng d
020 _aTHE0005923(Local)
039 9 _a201905141445
_baida
_c201107132323
_dVLOAD
_y201006031437
_zFida
040 _aUMP
090 _aTA480 .A6 F57 2009 rs Bc.
100 0 _aMohd Firdaus Mohd Zaid
245 1 0 _aInvestigation on the shear joints failure with tensile loading for aluminum pins /
_cMohd Firdaus Bin Mohd Zaid
246 3 _aInvestigation on the shear joints failure with tensile loading for aluminum pins
_h[electronic resource]
260 _aKuantan, Pahang :
_bUMP ,
_c2009
300 _axiv, 62 p. :
_bill. (some col.) ;
_c30 cm. + 1 computer disc
502 _aProject paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2009
504 _aBibliography : p. 52
520 _aThe use of pin joints is to connect two steel plates together and to support load together or alone. It has been extensively used in civil, mechanical and aircraft structures. Most of the available methods have been developed to estimate the loading capacity using side-edge distance but not the position of the pins using angle. In this paper, a research is developed to recommend the best position of pin group under in tensile loads based on the assumptions of angle and distance from centroid. The investigation is using Aluminum pins as connecter to joint two plates made of steel. The force applied on the side of plate and the Finite Element Analysis (ALGOR) as software to analysis the model. The analysis is use to find the lowest stress from four pins and that the first pins will fail. That means the pin can support lowest load than others pins. From the result, the pin closest to the load applied, not symmetry with other pin or alone and far from centroid axis are faster failed. As conclusion, The more close distance to centroid axis and other pins, to more higher maximum stress or the pin can support high load before it failed.
650 0 _aAluminum
999 _aVIRTUA40
_c1857
_d1863
999 _aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*9992