Title :
Notice of Retraction
3-D transient temperature field analysis for aircraft brake system
Author :
Yinghui Song ; Yuren Li ; Bo Liang
Author_Institution :
Sch. of Autom., Northwestern Polytech. Univ., Xi´an, China
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 order to catch the trend of temperature´s changing in the braking system more accurately. In this paper, thermodynamic principle to establish 3D finite element model. The calculating method of temperature field of brake during aircraft braking is put out. Discussed the boundary conditions and determined the various parameter. In order to know the 3D transient temperature field of aircraft braking in multiple load, ANSYS10.0 was applied to calculate the temperature field of braking. The simulation results are given as the temperature distribution and the keypoint temperature cure. The simulation results shows that this method is more accurate as well as effective.
Keywords :
aircraft; brakes; finite element analysis; mechanical engineering computing; temperature distribution; thermodynamics; 3D finite element model; 3D transient temperature field analysis; ANSYS10.0; aircraft brake system; boundary condition; keypoint temperature cure; temperature distribution; thermodynamic principle; Aircraft; Finite element methods; Heating; Mathematical model; Temperature distribution; Transient analysis; 3Dtransient temperature field; Brake system; Finite element analysis;
Conference_Titel :
Artificial Intelligence, Management Science and Electronic Commerce (AIMSEC), 2011 2nd International Conference on
Conference_Location :
Dengleng
Print_ISBN :
978-1-4577-0535-9
DOI :
10.1109/AIMSEC.2011.6010748
