摘要
A transition model, γ-Reθt-fRe, considering flow compressibility is developed from the original γ-Reθ ttransition model framework. The compressibility correction is introduced for the existing transition criteria, and the original transition correlation function based on incompressible flow is modified using the Reynolds number compressibility analogy relation obtained by the reference temperature method. To achieve model localization, an additional Reynolds number compressibility analogy relation fRe transport equation is constructed. The developed γ-Reθt-fRetransition model is used to examine the transition cases under different flow conditions and compared with the basic γ-Reθ ttransition model. The numerical simulation results show that the γ-Reθ t-fRe transition model achieves seamless unified simulation capability from low speed to high speed. It is automatically restored to the basic γ-Reθ ttransition model under low speed flow conditions, while significantly improves the prediction of the flow transition trigger position and transition zone development under supersonic and hypersonic flow conditions.
投稿的翻译标题 | γ-Reθt-fRetransition model for compressible flow |
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源语言 | 繁体中文 |
文章编号 | 125794 |
期刊 | Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica |
卷 | 43 |
期 | 8 |
DOI | |
出版状态 | 已出版 - 25 8月 2022 |
关键词
- compressibility correction
- flow transition
- hypersonic
- reference temperature method
- γ-Retransition model