A Spline-Based Stress Function Approach for the Principle of Minimum Complementary Energy
A Spline-Based Stress Function Approach for the Principle of Minimum Complementary Energy
In computational engineering, ensuring the integrity and safety of structures in fields such as aerospace and civil engineering relies on accurate stress prediction. However, analytical methods are limited to simple test cases, and displacement-based finite element methods (FEMs), while commonly used, require a large number of unknowns to achieve high accuracy; stress-based numerical methods have so far failed to provide a simple and effective alternative. This work aims to develop a novel numerical approach that overcomes these limitations by enabling accurate stress prediction with improved flexibility for complex geometries and boundary conditions and fewer degrees of freedom (DOFs). The proposed method is based on a spline-based stress function formulation for the principle of minimum complementary energy, which we apply to plane, linear elastostatics. The method is first validated against an analytical power series solution and then tested on two test cases challenging for current state-of-the-art numerical schemes, a bi-layer cantilever with anisotropic material behavior, and a cantilever with a non-prismatic, parabolic-shaped beam geometry. Results demonstrate that our approach, unlike analytical methods, can be easily applied to general geometries and boundary conditions, and achieves stress accuracy comparable to that reported in the literature for displacement-based FEMs, while requiring significantly fewer DOFs. This novel spline-based stress function approach thus provides an efficient and flexible tool for accurate stress prediction, with promising applications in structural analysis and numerical design.
Fabian Key、Lukas Freinberger
工程基础科学建筑基础科学航空航天技术
Fabian Key,Lukas Freinberger.A Spline-Based Stress Function Approach for the Principle of Minimum Complementary Energy[EB/OL].(2025-06-24)[2025-07-16].https://arxiv.org/abs/2506.19534.点此复制
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