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摘要:
In this paper, the optimization scheme of a centrifugal fan under the constraints of the total pressure difference, efficiency and shaft power was carried out. The blade inlet angle ?1A and the blade outlet angle ?2A of the centrifugal impeller were optimized using the Response Surface Methodology (RSM). Nine optimization cases were presented. The aerodynamic performance and the flow field of the optimized model were carefully compared with the original model. The results show that the total pressure difference and the total-pressure efficiency increase by 5.7% and 4.2% respectively after the optimization. Compared with the original fan, the flow field inside the impeller of the optimized fan has been improved. The flow separation existing around the blade suction surface outlet is suppressed significantly. For fields in the volute, the optimization scheme has reduced the local vortex intensity and weakened the vortex scale. The flow field stability around the volute tongue is also correspondingly improved.
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篇名 Aerodynamic Optimization of a Centrifugal Fan Using Response Surface Methodology
来源期刊 流体动力学(英文) 学科 医学
关键词 CENTRIFUGAL FAN OPTIMIZATION RESPONSE SURFACE METHODOLOGY
年,卷(期) ltdlxyw_2019,(1) 所属期刊栏目
研究方向 页码范围 92-105
页数 14页 分类号 R73
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研究主题发展历程
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CENTRIFUGAL
FAN
OPTIMIZATION
RESPONSE
SURFACE
METHODOLOGY
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研究去脉
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期刊影响力
流体动力学(英文)
季刊
2165-3852
武汉市江夏区汤逊湖北路38号光谷总部空间
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302
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