DocumentCode
524360
Title
Notice of Retraction
Numerical simulation on the plate based on wind tunnel tests
Author
Zihua Zhang ; Ping Wang
Author_Institution
Dept. of Phys. Educ., Tongren Univ., Tongren, China
Volume
3
fYear
2010
fDate
22-24 June 2010
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.
The problem of flowing around the plate in many different attacked angles has been simulated by Fluent 6.2 in this article. Through the analysis, it can be found that the results of resistance and lift at the angle of 40-60° are not satisfied, and it has been needed more analysis in those angles. The simulation on large and small attacked angles are much approached to the wind tunnel tests, and for large one, SST K-ω are suggested to be used; for small one, S-A or Standard k-ε are suggested to be used. The simulation of second up wind is more correct for the results.
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.
The problem of flowing around the plate in many different attacked angles has been simulated by Fluent 6.2 in this article. Through the analysis, it can be found that the results of resistance and lift at the angle of 40-60° are not satisfied, and it has been needed more analysis in those angles. The simulation on large and small attacked angles are much approached to the wind tunnel tests, and for large one, SST K-ω are suggested to be used; for small one, S-A or Standard k-ε are suggested to be used. The simulation of second up wind is more correct for the results.
Keywords
flow simulation; numerical analysis; plates (structures); wind tunnels; Fluent 6.2; SST K-ω model; flow simulation; plates; standard k-ε model; wind tunnel tests; Aerospace industry; Automotive components; Computer science education; Educational technology; Equations; Fluid dynamics; Fluid flow control; Numerical simulation; Shape measurement; Testing; attacked angles; calculation models; numerical simulation; plate;
fLanguage
English
Publisher
ieee
Conference_Titel
Education Technology and Computer (ICETC), 2010 2nd International Conference on
Conference_Location
Shanghai
Print_ISBN
978-1-4244-6367-1
Type
conf
DOI
10.1109/ICETC.2010.5529521
Filename
5529521
Link To Document