DocumentCode
1831227
Title
Notice of Retraction
Prediction of flow filed over half-span delta wings using backpropagation neural network
Author
Alibeigi, S. ; Sadati, S.H.
Author_Institution
Dept. of Mech. & Aerosp. Eng., I.A.U., Tehran, Tehran, Iran
Volume
2
fYear
2010
fDate
1-3 Aug. 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.
In this paper, a flow field of a half delta wing was predicted by using a neural network (NN). Backpropagation algorithm has been used to train the network. Data obtained from wind tunnel tests were used to train the network and for the verification of the NN values predicted. The simulation results and those of the experimental are in good agreement.
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.
In this paper, a flow field of a half delta wing was predicted by using a neural network (NN). Backpropagation algorithm has been used to train the network. Data obtained from wind tunnel tests were used to train the network and for the verification of the NN values predicted. The simulation results and those of the experimental are in good agreement.
Keywords
aerodynamics; aerospace components; backpropagation; mechanical engineering computing; neural nets; backpropagation neural network; flow field prediction; half-span delta wings; wind tunnel tests; Artificial neural networks; Lead; Half-span delta wing; backpropagation; neural network; vortex;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanical and Electronics Engineering (ICMEE), 2010 2nd International Conference on
Conference_Location
Kyoto
Print_ISBN
978-1-4244-7479-0
Type
conf
DOI
10.1109/ICMEE.2010.5558444
Filename
5558444
Link To Document