PDF(143 KB)
Optimal ratio of bend channel in centrifugal compressor
- WEN Suping1, HU Xiaowen1, LI Tingbin1, ZHANG Yong2, WANG Jun2
Author information
+
1.School of Energy and Power Engineering, Xi'an Jiaotong University; 2.Shenyang Blower Works
Show less
History
+
Published |
05 Dec 2008 |
Issue Date |
05 Dec 2008 |
{{custom_sec.title}}
{{custom_sec.title}}
{{custom_sec.content}}
This is a preview of subscription content, contact
us for subscripton.
References
1. Aungler R . Aerodynamicdesign and analysis of vaneless diffusers and return channels. ASME Paper No. 93-GT-101, New York, 1993
2. Davis W R . Three-dimensional boundary layer computation on the stationary end-wallsof centrifugal turbomachinery. T ASME JFluid Eng, 1976, 98: 431–442
3. Akaike S, Toyokura T . Flow in interstage returnbend of centrifugal turbomachinery. In: Kisbocskoi L, Szabo A, eds. Proceedings of the 6th Conference on Fluid Machinery . Budapest, Hungary, 1979, 11–20
4. Oh J M, Engeda A . A numerical study of theU-turn bend in return channel systems for multistage centrifugal compressors. J Mechanical Engineering Science, 2005, 219(8): 749–756
5. Inoue Y, Koizumi T . Experimental study on flowpatterns and losses in return passages for centrifugal compressor. ASME Fluid Eng Div, 1983, 3: 13–21
6. Lenke L J, Simon H . Numerical simulation of theflow through the return channel of multistage centrifugal compressors. In: 43rd IGTI-ASME Conference . Stockholm, Sweden, 1998, 10–19
7. Fister W, Zahn G, Tasche J . Theoretical and experimental investigations about vanelessreturn channels of multi-stage radial flow turbomachines. ASME paper 82-GT-209, 1982