DocumentCode
3369564
Title
Buckling analysis on finite-sized shell structures
Author
Liu, Jiantao ; Du, Pingan ; Huang, Mingjing ; Xiao, Yaobing
Author_Institution
Sch. of Mech. Eng., Univ. of Electron. Sci. & Technol. of China, Chengdu, China
fYear
2009
fDate
9-12 Aug. 2009
Firstpage
4267
Lastpage
4271
Abstract
The theoretical analysis of finite element method for buckling phenomenon to finite-sized shell structure is first introduced. Then, a real application using a probe for detecting the pressure inside turboprops is analyzed thoroughly with ANSYS10.0, including section profile, dimensions, and local characteristics. Based on the solved results, several rules between critical load and influence factors are obtained, which would be helpful for similar structures design and application. Finally, several useful conclusions about the best profile and ratio between dimensions are obtained.
Keywords
buckling; finite element analysis; jet engines; shells (structures); ANSYS10.0; buckling analysis; buckling phenomenon; finite element method; finite-sized shell structures; turboprops; Structural shells; Buckling deformation; Critical load; Curved shell structure; Eigenvalue buckling analysis; Finite Element Method;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location
Changchun
Print_ISBN
978-1-4244-2692-8
Electronic_ISBN
978-1-4244-2693-5
Type
conf
DOI
10.1109/ICMA.2009.5246529
Filename
5246529
Link To Document