DocumentCode :
523647
Title :
An Improved Finite Element Simulation Method for Plate Wrinkling
Author :
Liang, Ke ; Sun, Qin ; Shen, Xiaxia
Author_Institution :
Sch. of Aeronaut., Northwestern Polytech. Univ., Xi´´an, China
Volume :
1
fYear :
2010
fDate :
11-12 May 2010
Firstpage :
552
Lastpage :
555
Abstract :
An improved FEM simulation method of the plate wrinkling is proposed in this work. This method is easier and more effective as well. Reasonable and credible results can be obtained when this method is used to analyze the stability of a plate under a shear load. The practicability of the proposed method is validated further by simulating the instability behavior of the wing box under the aerodynamic force.
Keywords :
Aerodynamics; Analytical models; Automation; Biomembranes; Chemical technology; Computational modeling; Deformable models; Finite element methods; Stability analysis; Sun; FEM; instability; wing box; wrinkling;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Intelligent Computation Technology and Automation (ICICTA), 2010 International Conference on
Conference_Location :
Changsha, China
Print_ISBN :
978-1-4244-7279-6
Electronic_ISBN :
978-1-4244-7280-2
Type :
conf
DOI :
10.1109/ICICTA.2010.228
Filename :
5522757
Link To Document :
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