| 000 | 02474nam a2200265 a 4500 | ||
|---|---|---|---|
| 001 | vtls000045756 | ||
| 003 | KUKTEM | ||
| 005 | 20251114204426.0 | ||
| 008 | 100513t2009 my ao f m 000 0 eng d | ||
| 020 | _aTHE0006217(Local) | ||
| 039 | 9 |
_a201905161057 _baida _c201107132319 _dVLOAD _c201005131228 _dida _y201005131223 _zida |
|
| 040 | _aUMP | ||
| 090 | _aTJ254.5 .K45 2009 rs Bc. | ||
| 100 | 0 | _aMohamad Khidhir Masteki | |
| 245 | 1 | 0 |
_aSimulation of gaseous fuel injector nozzle angle effect on compressed natural gas (CNG) engine / _cMohamad Khidhir Masteki |
| 246 | 3 |
_aSimulation of gaseous fuel injector nozzle angle effect on compressed natural gas (CNG) engine _h[electronic resource] |
|
| 260 |
_aKuantan, Pahang : _bUMP, _c2009 |
||
| 300 |
_axvi, 61 p. : _bill. (some col.) ; _c30 cm. + _e1 computer disc |
||
| 502 | _aProject paper (Bachelor of Mechanical Engineering with Automotive Engineering) -- Universiti Malaysia Pahang - 2009 | ||
| 504 | _aIncludes bibliographical references | ||
| 520 | 3 | _aThe performance of an indirect injection (ID-I) compressed natural gas engine (CNG) is highly dependent on the quality of the air fuel mixture preparation. This is particular important when operating at a stratified charge condition, where ideal mixture distribution would form a homogenous region. And this has connection with the flow of injection. The study of flow pattern for injector nozzle is very important before the process is entering the real engine. Numerical simulation was carried out to investigate the effect of fluid motion of different angle nozzle in the injector. Other than investigate the fuel pattern, this project also recommend that the single nozzle hole of injector are not suitable for get a better mixing. Computational Fluid Dynamics application software (FLUENT), was used to simulate the fluid flow motion generated by different nozzle angle of injection. The analysis only was done in non-combustion bomb which is easy to identify the better flow which comes out from injector with a different angle. This project are simulated in two dimension modeling because the result can be obtain from two dimensional modeling, not in three dimension. The entire information and analysis in this thesis are hope could provide references for the future potential researchers. | |
| 650 | 0 | _aCombustion engineering | |
| 650 | 0 | _aNozzles | |
| 999 |
_aVIRTUA40 _c1817 _d1823 |
||
| 999 | _aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992 | ||