Supersonic starting jet impingements upon hemispherical concavities
A numerical study on starting supersonic jets impinging upon hemispherical concavities was conducted using OpenFOAM platform based on rhoCentralFoam transient compressible flow solver. Three concavities of diameter ratios of D / d = 0.5 , 1, and 2 were studied to understand how the flow and shock st...
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| Main Authors: | , , |
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| 其他作者: | |
| 格式: | Article |
| 語言: | English |
| 出版: |
2025
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| 主題: | |
| 在線閱讀: | https://hdl.handle.net/10356/184752 |
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| 機構: | Nanyang Technological University |
| 語言: | English |