02164nam a2200289 a 4500001001400000003000700014005001700021008004100038020002200079039008300101040000800184090003000192100002300222245007900245246007400324260003400398300006400432502012000496504002800616520080200644650003201446650002601478952012401504952013401628999002501762999008701787vtls000052799KUKTEM20251114204448.0110412t2010    my da  f m    000 0 eng d  aTHE0006294(Local) 9a201905161614baidac201110041233dFidac201107140045dVLOADy201104121357zida  aUMP  aTJ762.C66 I99 2010 rs Bc.0 aIzzul Izwan Ismail10aModal analysis of engine piston rod for small engine /cIzzul Izwan Ismail3 aModal analysis of engine piston rod for small engineh[computer file]  aKuantan, Pahang :bUMP,c2010  axiv, 54 p. :bill. (some col.) ;c30 cm. +e1 computer disc  aProject paper (Bachelor of Mechanical Engineering with Automotive Engineering) -- Universiti Malaysia Pahang - 2010  aBibliography : p. 47-483 aIn reciprocating small engine system, piston rod connects the piston and crankshafts. Piston rod is always under tremendous stress level created by load and force. It will produce great vibration. Sometimes the vibration is higher than the natural frequency of piston rod. This will lead to the piston rod failure in small engine. Situation which vibration frequency exceeding natural frequency is known as resonance. Finite element analysis and experimental modal analysis are two methods to investigate the dynamic behavior of piston rod and thus determining its natural frequency. Finite element analysis involved several mesh size. Result from both methods is compared and prominently discussed to achieve project objective. Finally, estimation of natural frequency and mesh size is suggested. 0aInternal combustion engines 0aFinite element method  00104071a20000b20000d2019-09-04l0oTJ762.C66 I99 2010 rs Bc.p0000054227r2019-09-04 00:00:00t1w2019-09-04yPSM  00104071a20000b20000d2019-09-04l0oCD 5129 | TJ762.C66 I99 2010 rs Bc.p0000054228r2019-09-04 00:00:00t1w2019-09-04yPSM  aVIRTUA40c2448d2454  aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992