摘要
The viscous flowfields of diffuser in altitude test cell were simulated based on the Reynolds-average unsteady Navier-Stodes equations with time-dependent method, MacCormack explicit scheme and Baldwin-Lomax algebraical turbulent model. The diffuser performance was calculated. The results show that the method of soluting Navier-Stokes equations is effective to predict the diffuser performance.
源语言 | 英语 |
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页(从-至) | 61-69 |
页数 | 9 |
期刊 | Tuijin Jishu/Journal of Propulsion Technology |
卷 | 19 |
期 | 6 |
出版状态 | 已出版 - 1998 |