The method of topology optimization was first implemented in the 1970s by Prager and Rozvany as Optimal Layout Theory. This theory was an extension to beam systems, or grillages, of the fundamental principles of topology optimization established by Michell, an Australian inventor, in 1904. This theory was then generalized considerably by Rozvany in the 1980s and 1990s. This theory was mainly aimed for low volume fractions.
Topology optimization for higher volume fractions is now often termed Generalized Shape Optimization (GSO). It consists of the simultaneous optimization of topology and shape of internal boundaries in porous and composite continua. In discrete mechanics, major early developments were influenced by the observations of Cheng and Olhoff in 1981, which stated that optimized solid plates contain systems of ribs which are similar to optimized grillages. In that same decade, for the compliance design of perforated plates in plane stress, optimal microstructures were studied with this method by various mathematicians.
The first exact analytical solutions for optimal perforated plates and the correct expressions for the rigidity tensor of homogenized optimal microstructures were obtained by Rozvany, Olhoff and Bendsoe in 1985-87, and by Ong, Rozvany and Szeto in 1988. Finite-element-based topology optimization for higher volume fractions was introduced by Bendsoe at the end of 1980s by extensive research, which set the basis for a ‘homogenization’ school of topology optimization (e.g. Bendsoe and Kikuchi 1988; Bendsoe, Diaz and Kikuchi 1993). A parallel exploration of the Solid Isotropic Microstructure with Penalization (SIMP) approach was originally suggested by Bendsoe in 1989, and later developed and named by Zhou and Rozvany in 1990-92.
In order to better understand the method behind topology optimization, one must understand what optimization is and what it aims to accomplish. The infographic below will give you a general definition.
Before topology optimization design, sizing optimization, which dealt only with the section coefficient of a structure, and shape optimization, which involved the modification of external appearance under given constraints, were the mainstream approach. Topology optimization differs in functionality in that it can be used even without an initial design, making it a very useful technique in the early phases of a product’s design.
For example, let us assume we are designing the cross section of the undercarriage of an airplane. By traditional methods, the required stiffness is achieved by reducing mass by drilling holes of appropriate size, and in appropriate quantity, within a rectangular cross section, but these values must be found by intuition and trial-and-error. When topology optimization is applied to this problem, however, it is possible to simultaneously find the number and shape of internal holes directly from the rectangle. Topology optimization makes it possible to satisfy design requirements to a high degree without the need of intuitive iterations.
Before performing topology optimization, it is necessary to understand geometric density, the one and only design variable in topology optimization. Geometric density is an imaginary value used to express the layout of material on a space. Referring to the picture below, elements on parts where the material should not be placed have a density of 0, or a small value close enough to 0, and parts where the material should be placed have a value of 1, or close enough to 1. According to this scale, if a geometric density of value between 0 and 1 is determined for all elements, the overall material distribution is determined.
Another important concept in topology optimization is sensitivity. When attempting to deduce a valid design by modifying design variables, the first thing to check is sensitivity. In general terms, sensitivity analysis is the study of how the uncertainty in the output of a mathematical model is influenced by different uncertainties in the model’s input. In the context of engineering optimization, sensitivity refers to how changes in the parameters and states, or design variables, of a model influence the optimization objective function.
For example, when a dimension (design variable) is changed from 1 to 3, if the target eigenvalue (objective function) increases from 5 Hz to 9Hz, maximizing the eigenvalue to be greater than 9 will mean the value of sensitivity is (9-5)/(3-1)=2. Therefore, to reach this optimization goal, the dimension will increase to more than 3 by factor of the sensitivity. Conversely, in a case involving minimizing the eigenvalue to be less than 5 HZ, sensitivity has a value of (5-9)/(3-1)=-2. This means the dimension will be reduced to less than 1 by a factor of sensitivity with respect to the eigenvalue.
In other words, sensitivity is the rate of change of the objective function in response to changes in the design variables. By this standard, the direction in which design variables are changed is determined.
If sensitivity is relatively high, the change in design variables is determined to be relatively large. However, the absolute size cannot be determined, and since sensitivity is also affected by any changes to the design variables, multiple repetitions are necessary before an optimum value can be deduced. And since topology optimization is carried out based on sensitivity, this method will also require multiple repetitions to determine the optimized topological layout.
Formulation of a Topology Optimization Problem
1. Objective Function
This is similar to selecting the analysis type. Since topology optimization can be used in linear static, modal and frequency response analyses, the analysis type appropriate for the design purpose should be selected.
For example, if the objective function is maximizing stiffness in response to a static load, linear static analysis should be selected. For maximization of the natural frequency of a structure, modal analysis is most appropriate. Finally, to improve stiffness in response to periodic dynamic loading, frequency response is usually selected.
Many other objective functions can be formulated for their respective analysis type depending on the design needs of the engineer.
2. Design Variables
Since the only design variable in topology optimization is the geometric density of the elements in the structure, a design set and non-design set can be determined with respect to the mesh to specify what elements will be subjected to optimization.
Elements that are included in the non-design set are still included in the analysis, but the geometric density is always kept as 1 to avoid optimization.
Elements without volume that are not 2D or 3D elements, such as springs, rigid bodies or masses, are automatically excluded from the analysis, even if the element is included in the design set.
If reduction of weight is the key objective, for example, volume is minimized using displacement or stress-limiting conditions. When maximizing stiffness at a set amount of material, volume ratio is selected as the constraint. For optimization stress-limiting conditions, there is almost no correlation between changes in maximum strength and overall amount of material. Therefore, the constraint is not the maximum stress but the average stress of all the elements.
For a framework type layout, optimization is usually attempted with a volume ratio around 30%. In an initial state where the mesh density is full, reduction of weight is only possible if the displacement or stress results in the constraint state are greater than the displacement or stress in the initial state.
That's how we got this shape...
This article is written by Gabriel Roade in MIDAS IT and published by Agnes Shin in MIDAS IT