New rational interpolation functions for finite element analysis of rotating beams


Autoria(s): Gunda, Jagadish Babu; Ganguli, Ranjan
Data(s)

01/03/2008

Resumo

A rotating beam finite element in which the interpolating shape functions are obtained by satisfying the governing static homogenous differential equation of Euler–Bernoulli rotating beams is developed in this work. The shape functions turn out to be rational functions which also depend on rotation speed and element position along the beam and account for the centrifugal stiffening effect. These rational functions yield the Hermite cubic when rotation speed becomes zero. The new element is applied for static and dynamic analysis of rotating beams. In the static case, a cantilever beam having a tip load is considered, with a radially varying axial force. It is found that this new element gives a very good approximation of the tip deflection to the analytical series solution value, as compared to the classical finite element given by the Hermite cubic shape functions. In the dynamic analysis, the new element is applied for uniform, and tapered rotating beams with cantilever and hinged boundary conditions to determine the natural frequencies, and the results compare very well with the published results given in the literature.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/26527/1/3.pdf

Gunda, Jagadish Babu and Ganguli, Ranjan (2008) New rational interpolation functions for finite element analysis of rotating beams. In: International Journal of Mechanical Sciences, 50 (3). pp. 578-588.

Publicador

Elsevier Science

Relação

http://www.sciencedirect.com/science?_ob=ArticleURL&_udi=B6V49-4PC3VVG-1&_user=512776&_coverDate=03%2F31%2F2008&_rdoc=1&_fmt=high&_orig=search&_sort=d&_docanchor=&view=c&_searchStrId=1266892420&_rerunOrigin=google&_acct=C000025298&_version=1&_urlVersion=0

http://eprints.iisc.ernet.in/26527/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed