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Isoparametric axisymmetric shell elements with temperature gradients for heat conduction
Affiliation:1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India;2. Pratt & Whitney Canada, Mississauga, Ontario L5T 1J3, Canada;3. Indian Institute of Petroleum, Dehradun 248005, India;1. Faculty of Mechanical Engineering, Brno University of Technology, Czech Republic;2. Provyko s.r.o, Czech Republic;3. Loughborough University, United Kingdom;1. Department of Aerospace Engineering, Indian Institute of Science, Bangalore 560012, India;2. Department of Mechanical Engineering, Indian Institute of Technology, Guwahati 781039, India
Abstract:This paper presents a finite element formulation for axisymmetric shell heat conduction where temperature gradients through the shell thickness are retained as primary nodal variables. The element geometry is constructed using the coordinates of the nodes lying on the middle surface of the shell and the middle surface nodal point normals. The element temperature field is approximated in terms of element approximation functions, the nodal temperature, and the nodal temperature gradients. The weak formulation of the two-dimensional Fourier heat conduction equation in cylindrical coordinate system is constructed. The finite element properties of the shell element are then derived using the weak formulation and the element temperature field approximation. The formulation permits linear temperature gradients through the shell thickness. Distributed heat flux as well as convective boundaries are permitted on all four faces of the element. Furthermore, the element can also have internal heat generation as well as orthotropic material properties. The superiority of the formulation in terms of efficiency and accuracy is demonstrated. Numerical examples are presented and a comparison is made with the theoretical results.
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