Cfd Simulation To Study The Effects Of Ribs In A Converging Nozzle Flow At Sonic Mach Number
The presence of a blunt base leads to flow separation in aerodynamic bodies, which causes a low-pressure in the wake region. At sonic Mach number, low pressure in the wake region contributes up to sixty percent of the total drag. This study is conducted to study the effect of the rectangular ribs...
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| Format: | Thesis |
| Language: | English |
| Published: |
2020
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| Online Access: | http://eprints.usm.my/47771/1/Cfd%20Simulation%20To%20Study%20The%20Effects%20Of%20Ribs%20In%20A%20Converging%20Nozzle%20Flow%20At%20Sonic%20Mach%20Number.pdf http://eprints.usm.my/47771/ |
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