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: | New, Tze How, You, Rion Guang Yi, Chan, Wai Lee |
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其他作者: | School of Mechanical and Aerospace Engineering |
格式: | Article |
語言: | English |
出版: |
2025
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在線閱讀: | https://hdl.handle.net/10356/184752 |
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