2019
DOI: 10.1002/nme.6148
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A novel minimum weight formulation of topology optimization implemented with reanalysis approach

Abstract: In this paper, we develop an efficient diagonal quadratic optimization formulation for minimum weight design problem subject to multiple constraints. A high-efficiency computational approach of topology optimization is implemented within the framework of approximate reanalysis. The key point of the formulation is the introduction of the reciprocal-type variables. The topology optimization seeking for minimum weight can be transformed as a sequence of quadratic program with separable and strictly positive defin… Show more

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Cited by 24 publications
(11 citation statements)
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“…Currently, a variety of optimizers are available in the topology optimization community. For instance, the compliance minimization problems involving sole volume constraint can be effectively resolved using heuristic optimality criteria and rigorous mathematical programming, e.g., the method of moving asymptotes (MMA) [ 53 ] and sequential quadratic programming (SQP) [ 54 , 55 ]. The introduction of the Lagrange multiplier to satisfy the constraint equation is nothing new in the level set method (LSM) [ 56 ] and the Bi-directional Evolutionary Structural Optimization (BESO) method [ 57 , 58 ].…”
Section: Optimization Problem For Infill Structurementioning
confidence: 99%
“…Currently, a variety of optimizers are available in the topology optimization community. For instance, the compliance minimization problems involving sole volume constraint can be effectively resolved using heuristic optimality criteria and rigorous mathematical programming, e.g., the method of moving asymptotes (MMA) [ 53 ] and sequential quadratic programming (SQP) [ 54 , 55 ]. The introduction of the Lagrange multiplier to satisfy the constraint equation is nothing new in the level set method (LSM) [ 56 ] and the Bi-directional Evolutionary Structural Optimization (BESO) method [ 57 , 58 ].…”
Section: Optimization Problem For Infill Structurementioning
confidence: 99%
“…For solving (2), the finite element (FE) method is used to calculate the objective function and sensitivity information at each iteration. The optimization criterion method or the method of moving asymptotes [27][28][29][30], combined with the sensitivity information to update the design variables until the convergence condition is met. Through the topological optimization design of the minimum mass under stress constraints, the material in the non-critical areas of the spacecraft rib can be reduced, and its load-bearing rate can be improved to a certain extent.…”
Section: Topology Optimization Of the Stress-constrained Mass Minimummentioning
confidence: 99%
“…The aforementioned studies have provided valuable algorithmic-level contributions to the goal of maximizing design resolution at an acceptable cost. Owing to the rapid development of computer science, several studies have used advanced algorithms or hardware (including GPU and supercomputers) to achieve the required high-resolution design [49][50][51][52]. Algorithm development and hardware update are complementary, not contradictory.…”
Section: Introductionmentioning
confidence: 99%