Abstract
The purpose of this study is to calculate the torsional rigidity and maximum shear stresses of arbitrarily shaped orthotropic composite or functionally graded material sections on the basis of a hybrid finite element approach. A hybrid finite element based on a Hellinger–Reissner functional is presented. A set of numerical examples is solved to verify the proposed method, and a parametrical study is also performed.
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Abbreviations
- D :
-
Diameter
- \(G_{zx},G_{zy}\) :
-
Shear modulus of elasticity
- \(G_{zy}^b , G_{zy}^t\) :
-
Shear moduli at the bottom and top sides of an FGM section
- GJ :
-
Torsional rigidity
- \(Q_{x},\,Q_{y}\) :
-
Internal shear force components
- T :
-
Torsional moment
- \(\beta \) :
-
Torsional rigidity factor
- \(\phi \) :
-
Saint-Venant’s stress function
- \(\theta \) :
-
Angle of twist per unit length
- \(\bar{{\tau }}_{\max }\) :
-
Maximum shear stress factor
- [D]:
-
Differential operator matrix
- [G]:
-
Nodal forces corresponding to assumed stress field
- [N]:
-
Shape functions
- [P]:
-
Interpolation matrix for stress
- \(\{q\}\) :
-
Displacement components
- \(\{w\}\) :
-
Displacements
- \(\{\beta \}\) :
-
Stress parameters
- \(\{\sigma \}\) :
-
Internal forces
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Darılmaz, K., Orakdöğen, E. & Girgin, K. Saint-Venant torsion of arbitrarily shaped orthotropic composite or FGM sections by a hybrid finite element approach. Acta Mech 229, 1387–1398 (2018). https://doi.org/10.1007/s00707-017-2067-1
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DOI: https://doi.org/10.1007/s00707-017-2067-1