Aissa, W., Eissa, M., Abdel-Fadeel, W., Mohamed, I. (2009). EXPERIMENTAL AND NUMERICAL STUDY OF LOW ASPECT RATIO ASYMMETRIC DIFFUSER. JES. Journal of Engineering Sciences, 37(No 2), 363-374. doi: 10.21608/jesaun.2009.125350
W. A. Aissa; M. S. Eissa; W. A. Abdel-Fadeel; I. K. Mohamed. "EXPERIMENTAL AND NUMERICAL STUDY OF LOW ASPECT RATIO ASYMMETRIC DIFFUSER". JES. Journal of Engineering Sciences, 37, No 2, 2009, 363-374. doi: 10.21608/jesaun.2009.125350
Aissa, W., Eissa, M., Abdel-Fadeel, W., Mohamed, I. (2009). 'EXPERIMENTAL AND NUMERICAL STUDY OF LOW ASPECT RATIO ASYMMETRIC DIFFUSER', JES. Journal of Engineering Sciences, 37(No 2), pp. 363-374. doi: 10.21608/jesaun.2009.125350
Aissa, W., Eissa, M., Abdel-Fadeel, W., Mohamed, I. EXPERIMENTAL AND NUMERICAL STUDY OF LOW ASPECT RATIO ASYMMETRIC DIFFUSER. JES. Journal of Engineering Sciences, 2009; 37(No 2): 363-374. doi: 10.21608/jesaun.2009.125350
EXPERIMENTAL AND NUMERICAL STUDY OF LOW ASPECT RATIO ASYMMETRIC DIFFUSER
1Mechanical Power Department, High Institute of Energy, South Valley University, Aswan, Egypt.
2Assistant Professor, Mechanical Power Department, High Institute of Energy, South Valley University, Aswan, Egypt Tel/Fax: +[20] 97 3480450
Abstract
The goal of the present study is to investigate the flow through an asymmetric low aspect ratio planar diffuser. The flow which is fully developed channel flow inlet conditions is both experimentally investigated and computed using commercial cfd code, fluent. Rng k- model is used as a turbulence model and standard wall function is used. The questions about the two-dimensionality of the flow are investigated. The Reynolds number of diffuser inlet flow is 3.5 x 105 based on the centerline velocity and the channel height. Flow is visualized to get insight view of the flow map in the diffuser.
View on SCiNiTO
Top