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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書目詳細資料
主要作者: Khan, Ambareen
格式: Thesis
語言:English
出版: 2020
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在線閱讀:http://eprints.usm.my/47771/1/Cfd%20Simulation%20To%20Study%20The%20Effects%20Of%20Ribs%20In%20A%20Converging%20Nozzle%20Flow%20At%20Sonic%20Mach%20Number.pdf
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