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