摘要
The work develops a localized hypersonic cross-flow transition criterion considering the influence of cross-flow intensity and surface roughness. A cross-flow extension of hypersonic modified ?-Re ? transition model based on Chant2.0 computing platform is implemented. The extended transition model is used to predict the cross-flow transition on the elliptic cone (HIFiRE-5) in multiple states, and the predicted results are in good accordance with the experimental results.
| 源语言 | 英语 |
|---|---|
| 文章编号 | 012051 |
| 期刊 | Journal of Physics: Conference Series |
| 卷 | 1786 |
| 期 | 1 |
| DOI | |
| 出版状态 | 已出版 - 24 2月 2021 |
| 活动 | 2020 11th Asia Conference on Mechanical and Aerospace Engineering, ACMAE 2020 - Chengdu, Virtual, 中国 期限: 25 12月 2020 → 27 12月 2020 |
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