DocumentCode
525842
Title
Notice of Retraction
The analysis of tip flow field in a centrifugal compressor with different circumferential grooves casing treatment
Author
Peng Gao ; Shiying Zhang
Author_Institution
Xi´an Res. Inst. of Hi-Tech, Xi´an, China
Volume
1
fYear
2010
fDate
12-13 June 2010
Firstpage
21
Lastpage
24
Abstract
Notice of Retraction
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
To research performance verify of the high speed centrifugal compressor between the two different conditions with the different circumferential grooves and with untreated smooth wall, the 3-dimentional numerical simulations were performed in a high speed centrifugal compressor with the 8 different circumferential grooves casing treatment. Detailed analyses of the flow visualization at the tip of blades have exposed the different tip flow topologies between these casings. It is concluded that the major reason of the mechanism of stall margin Improvement is restrained the tip leakage vortex.
After careful and considered review of the content of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE´s Publication Principles.
We hereby retract the content of this paper. Reasonable effort should be made to remove all past references to this paper.
The presenting author of this paper has the option to appeal this decision by contacting TPII@ieee.org.
To research performance verify of the high speed centrifugal compressor between the two different conditions with the different circumferential grooves and with untreated smooth wall, the 3-dimentional numerical simulations were performed in a high speed centrifugal compressor with the 8 different circumferential grooves casing treatment. Detailed analyses of the flow visualization at the tip of blades have exposed the different tip flow topologies between these casings. It is concluded that the major reason of the mechanism of stall margin Improvement is restrained the tip leakage vortex.
Keywords
blades; compressors; flow simulation; numerical analysis; packaging; vortices; blades; centrifugal compressor; circumferential grooves casing treatment; flow visualization; numerical simulations; tip flow field; tip leakage vortex; Hemorrhaging; Impellers; Numerical models; Topology; centrifugal compressor; circumferential grooves casing treatment; stall margin; tip leakage vortex;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer and Communication Technologies in Agriculture Engineering (CCTAE), 2010 International Conference On
Conference_Location
Chengdu
Print_ISBN
978-1-4244-6944-4
Type
conf
DOI
10.1109/CCTAE.2010.5543690
Filename
5543690
Link To Document