Sentence examples for minimum compliance optimization from inspiring English sources

The paper proposes a simple implementation for minimum compliance optimization relying on the finite element library and analysis capabilities of a commercial FEM-code and its Application Programming Interface.

With local ceramic volume fraction and lamella orientation chosen as the design variables, a minimum compliance optimization problem is solved based on topology optimization and finite element methods for metal ceramic samples with different geometries and boundary conditions.

To account for this feature this paper presents a novel method for generating simultaneously optimized shell and infill in the context of minimum compliance topology optimization.

Petersson et al. [14] considered the problem of minimum compliance topology optimization of an elastic continuum.

This paper presents a novel method for including coated structures and prescribed material interface properties into the minimum compliance topology optimization problem.

The suggested approach thereby addresses an important inadequacy of the standard minimum compliance topology optimization approach, in which buckling is rarely accounted for; rather, a satisfactory buckling load is usually assured through a post-processing step that may lead to sub-optimal components.

The performance of our approach is studied on few illustrative examples, including the optimization of engineered constructions for the minimum compliance and the optimization of the microstructure of a metamaterial for the desired macroscopic tensor of elasticity.

This paper proposes a novel adaptive volume constraint algorithm (AVC) to replace the fixed volume constraint (FVC) in the traditional topology optimization method, such that a minimum-compliance optimal structure that simultaneously meets the additional displacement limit can be searched.

We present a fully adaptive finite element scheme, named ATOPT algorithm, to address topology optimization for minimum compliance.

The technique is demonstrated on classic topology optimization problems including minimum compliance, heat conduction, and compliant mechanisms.

The optimal layout design of the space vehicle structure considering attitude control effort is, thus, reformulated as a topology optimization problem for minimum compliance under constraints on mass moments of inertia.