DocumentCode :
609230
Title :
Finite element analysis on curved beams of various sections
Author :
Mathiyazhagan, G. ; Vasiraja, N.
Author_Institution :
Dept. of Mech. Eng., Mepco Schlenk Eng. Coll., Sivakasi, India
fYear :
2013
fDate :
10-12 April 2013
Firstpage :
168
Lastpage :
173
Abstract :
Beam elements have played a very important role in modeling mechanical engineering structures. Curved beams are known to be more efficient in transfer of loads than straight beams. The transfer in the curved beam is affected by means of bending, shear and membrane action. This is particularly important in studying initially curved beams. The aim of this project is to improve the use and flexibility of curved beams in various mechanical components and structures. In this project the finite element formulation is used to analyze static and dynamic analysis of a curved cantilever beam with various cross sections, various types of curvature under various types of load and its directions, for linear elastic isotropic materials. The numerical analysis for the beam is solved by means of ANSYS and the deflection values are tabulated.
Keywords :
beams (structures); bending; cantilevers; elasticity; finite element analysis; structural engineering; ANSYS; beam elements; beam numerical analysis; bending; curved beam flexibility; curved cantilever beam; deflection values; dynamic analysis; finite element analysis; finite element formulation; linear elastic isotropic materials; load transfer; mechanical components; mechanical engineering structures; membrane action; shear; static analysis; Analytical models; Finite element analysis; Load modeling; Materials; Mathematical model; Numerical models; Stress; Curved cantilever beam; linear-elastic isotropic materials; static analysis;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Energy Efficient Technologies for Sustainability (ICEETS), 2013 International Conference on
Conference_Location :
Nagercoil
Print_ISBN :
978-1-4673-6149-1
Type :
conf
DOI :
10.1109/ICEETS.2013.6533377
Filename :
6533377
Link To Document :
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