Generalized Multifield Variational Sectional Analysis of Composite Blades Considering Nonuniform Torsion

F-0072-2016-11550

5/17/2016

Authors
Abstract
Content

A finite element (FE) cross-sectional analysis is developed based on the Reissner's multifield variational principle to model the three-dimensional (3D) warping displacements and sectional stresses. The classical elastic couplings are taken into account along with the rigorous treatment of nonclassical couplings due to nonuniform torsional warping. The in- and out-of-plane warping displacements, and sectional stresses are approximated as linear functions of generalized sectional stress resultants at the global level, and using FE shape functions at the local sectional level. A generalized Timoshenko-Vlasov level 7 x 7 stiffness matrix is formulated which incorporates Timoshenko like model for bending, and Vlasov like model for restrained torsion. The accuracy of the present analysis is substantiated using a variety of benchmark composite beams and rotor blades. The present results show a good correlation compared with other state-of-the-art methods, 3D FE analysis and/or experimental data.

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DOI
https://doi.org/10.4050/F-0072-2016-11550
Citation
Dhadwal, M. and Jung, S., "Generalized Multifield Variational Sectional Analysis of Composite Blades Considering Nonuniform Torsion," Vertical Flight Society 72nd Annual Forum and Technology Display, West Palm Beach, Florida, May 17, 2016, https://doi.org/10.4050/F-0072-2016-11550.
Additional Details
Publisher
Published
5/17/2016
Product Code
F-0072-2016-11550
Content Type
Technical Paper
Language
English