首页|基于三维体积力模型的离心压气机喘振预测方法

基于三维体积力模型的离心压气机喘振预测方法

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为了实现对喘振流动现象的准确、快速预测,提出了一种基于三维体积力模型的离心压气机喘振预测方法,并在一款跨声速离心压气机上进行了应用,对以叶轮进口叶尖"回流泡"、喘振中的旋转失速,以及蜗壳诱发的非对称流动为代表的典型喘振流场结构进行了捕捉.通过与经试验校核的全三维非定常雷诺平均Navier-Stokes(URANS)方法进行对比表明:本文提出的离心压气机喘振预测方法,针对主要喘振流动特征的预测具备与全三维URANS方法相当的能力,同时计算时间约为全三维URANS方法的1/20.
Surge prediction of radial compressors based on three-dimensional body-force method
To predict the three-dimensional and unsteady flow features of surge accurately and efficiently,a method of surge simulation for centrifugal compressors based on the three-dimensional body-force model was proposed.The method was further validated on a transonic centrifugal compressor.Typical flow field features like the development of the recirculation bubble at the impeller inlet tip,the existence of rotating stall during surge,and volute-induced asymmetry were captured.By comparing against the unsteady Reynolds averaged Navier-Stokes(URANS)results(validated by the experimental results),it can be shown that the proposed method is capable of predicting key features of surge,with the calculation time about 1/20 of the URANS method.

centrifugal compressorsurgebody-force modelmodeling methodunsteady Reynolds averaged Navier-Stokes method

曾翰轩、范腾博、温孟阳、魏杰、王钧莹、孙振中、郑新前

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清华大学车辆与运载学院,北京 100084

清华大学航空发动机研究院,北京 100084

离心压气机 喘振 体积力模型 模拟方法 非定常雷诺平均Navier-Stokes方法

国家科技重大专项国家科技重大专项

2017-Ⅱ-0004-0016J2019-Ⅰ-0011

2024

航空动力学报
中国航空学会

航空动力学报

CSTPCD北大核心
影响因子:0.59
ISSN:1000-8055
年,卷(期):2024.39(2)
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