 Research article
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Stressconstrained topology optimization using approximate reanalysis with onthefly reduced order modeling
Advanced Modeling and Simulation in Engineering Sciences volume 9, Article number: 17 (2022)
Abstract
Most of the methods used today for handling local stress constraints in topology optimization, fail to directly address the nonselfadjointness of the stressconstrained topology optimization problem. This in turn could drastically raise the computational cost for an already largescale problem. These problems involve both the equilibrium equations resulting from finite element analysis (FEA) in each iteration, as well as the adjoint equations from the sensitivity analysis of the stress constraints. In this work, we present a paradigm for largescale stressconstrained topology optimization problems, where we build a multigrid approach using an onthefly Reduced Order Model (ROM) and the pnorm aggregation function, in which the discrete reducedorder basis functions (modes) are adaptively constructed for adjoint problems. In addition to reducing the computational savings due to the ROM, we also address the computational cost of the ROM learning and updating phases. Both reducedorder bases are enriched according to the residual threshold of the corresponding linear systems, and the grid resolution is adaptively selected based on the relative error in approximating the objective function and constraint values during the iteration. The tests on 2D and 3D benchmark problems demonstrate improved performance with acceptable objective and constraint violation errors. Finally, we thoroughly investigate the influence of relevant stress constraint parameters such as the p norm factor, stress penalty factor, and the allowable stress value.
Introduction
Mechanical stress is a critical factor that affects performance, service life, fatigue resistance and safety of structural components, and is inarguably an important design criterion. Traditional topology optimization formulations (such as the minimum compliance problem with a volume constraint [1,2,3]) typically do not consider stress constraints, which could result in the phenomenon of high stress concentrations, leading to a final ”optimized” design that all too often fails to meet real engineering requirements, eventually requiring manual adjustment or shape optimization as a subsequent step.
In the past two decades, many researchers have worked on stressconstrained topology optimization [4, 5] in order to ensure that the design results are closer to engineering reality. However, when compared with the stressconstraintfree problem, stressconstrained topology optimization design presents a unique set of difficulties, which may be broadly classified as follows:

1.
The stress singularity phenomenon. This was first studied for the truss optimization problem. Cheng and Jiang [6, 7] gave a mathematical explanation for the singularity in the topology optimization problem, attributing it to the discontinuity of the stress constraint. Duysinx and Bendsøe [8] linked stress singularity to the phenomenon of nonvanishing stresses as the design variables tended towards zero, in other words, a region with a very small relative density could end up with a nonzero strain which then gives rise to nonzero (or even very high) stress, despite the fact that it represents a hole (void area). Today, the singularity problem is typically resolved by adopting therelaxation approach [7,8,9], QPrelaxation method [10] and stress penalization [11].

2.
Large number of local stress constraints. Since stress is a local parameter, the greater the number of elements for the domain discretization, the more there will be stress evaluation points, resulting in a large number of local nonconvex stress constraints, which in turn will lead to a steep rise in computational cost for the sensitivity analysis of local stress constraints [4, 12]. To reduce the computational complexity, local stress constraints are usually transformed into a global stress constraint or some form of clusterbased stress constraints by using a condensation function that approximates the value of the maximum local function. Currently, the two most common types of condensation functions are the KreisselmeierSteinhauser function (KS) [4, 12,13,14,15,16] and the Pnorm function [9, 16,17,18], and they can merge a mass of local stresses into a single constraint formula.

3.
Highly nonlinear nature of the stress constraint. Any change in density value of the adjacent region will significantly affect the stress level within some key regions [13, 17] such as depressions and corners. This requires the optimization procedure to be able to effectively reduce or eliminate the stress concentration phenomenon, and that the solution algorithm must maintain numerical consistency with the optimization procedure in order to ensure stable convergence of the overall procedure [19, 20].
In view of the three broad classes of problems associated with stressbased topology optimization listed above, researchers have put forward a variety of effective methods to deal with them.
However, with modernday sophisticated numerical methods and the recent development of advanced manufacturing technologies, the performance requirements for mechanical parts in the aerospace industry have become increasingly demanding [21]. Modeling with highly refined finite element models typically results in a series of ultralargescale problems with degrees of freedom ranging from tens of millions to even billions. Given the presence of nonconvex, nonlinear stress constraints in largescale topology optimization, the main hindrances then are the solution of largescale linear systems during the FEA analysis (equilibrium equation) in each iteration, as well as the sensitivity analysis of stress constraint functions due to the non selfadjoint nature [22]. Stress coagulation alone is then inadequate to improve the design, meaning that we need another approach [23].
One highly effective and proven solution is Approximate Reanalysis (AR) using a Reduced Order Model (ROM) technique [24,25,26,27]. Due to the nonselfadjointness of the problem, we need to solve two highdimensional systems during each iteration of the optimization process, the first being the equilibrium equations from finite element analysis (FEA), the other being the adjoint equations for the sensitivity analysis of the stress constraints. To the authors’ knowledge, virtually no work has been reported on coupling stressconstrained topology optimization with approximate reanalysis using a ROM.
In this work, we first apply two previously proposed ROM approaches to the stressconstrained topology optimization problem, the first being onthefly ROM using Principal Components Analysis (PCA) [28] and the other being multifidelity ROM using the multigrid method (MG) [29]. In addition, based on the proposed multifidelity ROM, we develop two improved strategies for further reductions in computational costs, the first one being the AdapROM where the residual threshold for the approximate solution of the equilibrium equations can be adaptively selected according to the relative error of the objective function value during the iteration; the second strategy being BiROM where we simultaneously apply the ROM to both the equilibrium equations and adjoint equations (during the sensitivity analysis of the stress constraint). Instead of the classical Optimality Criteria (OC) method, the Method of Moving Asymptotes (MMA) [30] is used as the optimization algorithm in this work, and the Pnorm function in [9] is adopted for coagulating the local stress constraints to reduce the computational cost involved. The stress singularity phenomenon is avoided by using stress penalization as in [11]. Recent years there are more papers about stress constraint [31,32,33].
This paper is organized in the following manner: in “Theoretical formulation”, the theoretical formulation is presented with a classical minimum compliance problem constrained by both stress and volume, followed by adjoint equationbased sensitivity analysis of both the objective function and the stress constraint function. “Projectionbased ROM approaches” first introduces two projectionbased ROM approaches including onthefly ROM construction using PCA and multifidelity ROM construction using the multigrid method, then combines both approaches into a single algorithm. In “Two improved strategies”, we propose two improved strategies (i.e. AdapROM and biROM). “Numerical tests” details the numerical investigations using a benchmark 2D Lshaped beam example. In “3D Lshaped beam”, we first apply a variety of ROM methods to the 3D compliance minimization problem of Lshaped beam, and then analyze the impact of the p norm factor p, the stress penalty factor q and the allowable maximum stress value \(\hat{\sigma }\) on the design results. The paper ends with discussion, concluding comments and recommendations for future work.
Theoretical formulation
Topology optimization model
The essence of topology optimization is mathematically determining the distribution of material in a geometrically fixed design domain under a set of constraints, such that the resulting structure achieves some optimal combination of mechanical performance objectives. Here, we consider the classical minimum compliance problem under stress and volume constraints, expressed as follows:
where, \(\varvec{\rho }\) is the vector consisting of the design variables (i.e. element (e) density), and \(N_{e}\) is the total number of design variables.denotes the compliance of the structure (objective function), \(\varvec{f}\) and \(\varvec{u}\) are external load vector and displacement vector of the structure respectively, \(\varvec{K}\) is the global stiffness matrix of the structure.\(V_{e}\) is the volume of element e and \(V_{0}\) is the initial volume of the structure, occupying the entire design domain,\(v_{f}\) and \(\hat{v}_{f}\) is the material volume fraction and its allowable value respectively. \(\sigma _{e}^{v M}\) represents the von Mises stress for an arbitrary element, \(\sigma _{e}^{v M}\) and \(\hat{\sigma }\) are the maximum von Mises stress of structure and its constraint limit value.
To suppress the generation of gray elements (intermediate values between 0 and 1) and obtain a clear blackandwhite pattern, we use a modified solid isotropic material with penalization (SIMP) interpolation [31], where the stiffness is penalized by a power function relation between the Young’s modulus \(E_{e}\) and element relative density \(\rho _{e}\), given by:
where, \(\omega >1\) is the SIMP penalty factor.is the Young’s modulus of solid material while \(E_{\min }\) is a vanishingly small positive value to avoid numerical instabilities such as a singular global stiffness matrix. In this paper, \(\omega \) assumes an empirical value of 3 while \(E_{\min }=10^{9}\).
To alleviate the singular solution problem, in a manner similar to stiffness penalization in SIMP model, we penalize the stress vectorin following scheme [12]:
where, \(q<1\) is the stress penalty factor, \(\varvec{D_{0}}\) is the constitutive matrix of solid materials and \(\varvec{B}\) is straindisplacement matrix. \(\sigma ^{0}_{e}=\varvec{D_{0}Bu_{e}}\) is the stress vector (Voight notation) calculated at the geometric center of the FE element (e), and the \(\sigma ^{0}_{e}\) has a different form in 2D and 3D case, which is given by:
The corresponding von Mises stressis then calculated as follows [34]:
In order to reduce the calculation cost caused by massive local stress constraints, we adopt the Pnorm function [14] to coagulate the \(N_{e}\) local stress constraints in Eq. (1) so that to form a global stress constraint, given by:
where, p may be interpreted as the Pnorm factor. And it determines the difference between the original function and its approximate value. When larger values are used, more weight is given to peak stress. Theoretically, as the value of the parameter p approaches infinity, we have:
Thus, the global stress constraint in Eq. (1) is transformed into,
However, it’s impossible to choose an infinite value of p and global measure function \(\sigma ^{PN}\) may not approximate \(\sigma _{\max }^{vM}\) very well. Therefore, we use following Eq. (8) to modify the constraint in Eq. (7),
where, adjusted parameter \(\xi =\sigma _{\max }^{vM}/\sigma ^{PN}\).
Generally, a high value of p could create problems with numerical accuracy since \(\sigma _{e}^{v M})^{P}\) could be very large. Actually when a high value of is used, the peak stress is weighted more heavily, it often leads to oscillation or even divergence during the optimization iterations. The oscillation results from the high nonlinearity of the global stress function. One workaround is to normalize the stress constraint, which is given by:
Sensitivity analysis
Using the adjoint method, the sensitivity of the objective function in Eq. (1) can be elegantly derived as follows:
where, Eq. (10) is the wellknown selfadjoint gradient as seen in [29].
Using the chain rule, we obtain the sensitivity of the stress constraint function \(\tilde{\sigma }^{PN}_{norm}\)
where, the three terms are respectively calculated as follows:

1.
the derivative of normalized Pnorm function with respect to von Mises stress.
$$\begin{aligned} \begin{aligned} \frac{\partial \tilde{\sigma }_{n o r m}^{P N}}{\partial \sigma _{e}^{v M}}&=\frac{\xi }{p \hat{\sigma }}\left( \sum _{e=1}^{N_{e}}\left( \frac{\sigma _{e}^{v M}}{\hat{\sigma }}\right) ^{p}\right) ^{\left( \frac{1}{p}1\right) }\times p\left( \frac{\sigma _{e}^{v M}}{\hat{\sigma }}\right) ^{p1} \\&=\frac{\xi }{\hat{\sigma }}\left( \sum _{e=1}^{N_{e}}\left( \frac{\sigma _{e}^{v M}}{\hat{\sigma }}\right) ^{p}\right) ^{\left( \frac{1}{p}1\right) } \times \left( \frac{\sigma _{e}^{v M}}{\hat{\sigma }}\right) ^{p1}. \end{aligned} \end{aligned}$$(13) 
2.
The derivative of the von Mises stress with respect to stress components. For the 2D case:
$$\begin{aligned} \left\{ \begin{array}{l} \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e x}}=\frac{1}{2 \sigma _{e}^{v M}}\left( 2 \sigma _{e x}\sigma _{e y}\right) \\ \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e y}}=\frac{1}{2 \sigma _{e}^{v M}}\left( 2 \sigma _{e y}\sigma _{e x}\right) \\ \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e z}}=\frac{2\tau _{exy}}{\sigma _{e}^{v M}}.\\ \end{array}\right. \end{aligned}$$(14)For the 3D case:
$$\begin{aligned} \left\{ \begin{array}{l} \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e x}}=\frac{1}{2 \sigma _{e}^{v M}}\left( 2 \sigma _{e x}\sigma _{e y}\sigma _{e z}\right) \\ \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e y}}=\frac{1}{2 \sigma _{e}^{v M}}\left( 2 \sigma _{e y}\sigma _{e x}\sigma _{e z}\right) \\ \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e z}}=\frac{1}{2 \sigma _{e}^{v M}}\left( 2 \sigma _{e z}\sigma _{e x}\sigma _{e y}\right) \\ \frac{\partial \sigma _{e}^{v M}}{\partial \tau _{e x y}}=\frac{3 \tau _{e x y}}{\sigma _{e}^{v M}}, \frac{\partial \sigma _{e}^{v M}}{\partial \tau _{e y z}}=\frac{3 \tau _{e y z}}{\sigma _{e}^{v M}}, \frac{\partial \sigma _{e}^{v M}}{\partial \tau _{e z x}}=\frac{3 \tau _{e z x}}{\sigma _{e}^{v M}}. \end{array}\right. \end{aligned}$$(15) 
3.
The derivative of the stress components with respect to the design variables:
$$\begin{aligned} \frac{\partial {\sigma _{e}}}{\partial \rho _{e}}=q\rho _{e}^{q1}\varvec{D_{0}Bu_{e}}+\rho _{e}^{q}\varvec{D_{0}B}\frac{\partial \varvec{u}_{e}}{\partial \rho _{e}}, \end{aligned}$$(16)where, the term \(\frac{\partial \varvec{u}_{e}}{\partial \rho _{e}}\) is obtained from the equilibrium equations:
$$\begin{aligned} \varvec{Ku=f}. \end{aligned}$$(17)By calculating the derivative of both sides of this equation, we have:
$$\begin{aligned} \frac{\partial \varvec{K}}{\partial \rho _{e}}\varvec{u_{e}}+\varvec{K}\frac{\partial \varvec{u_{e}}}{\partial \rho _{e}}=\varvec{0}. \end{aligned}$$(18)Giving,
$$\begin{aligned} \frac{\partial \varvec{u_{e}}}{\partial \rho _{e}}=\varvec{K}^{1}\frac{\partial \varvec{K}}{\partial \rho _{e}}\varvec{u_{e}}. \end{aligned}$$(19)Substituting Eq. (18) into Eq. (15) and then Eq. (15) into Eq. (11) gives,
$$\begin{aligned} \frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \rho _{e}}=\frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \sigma _{e}^{v M}}\left( \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e}}\right) ^{T} \times \left( q \rho _{e}^{q1} \varvec{D}_{0} \varvec{B} \varvec{u}_{e}\rho _{e}^{q} \varvec{D}_{0} \varvec{B} \varvec{K}^{1} \frac{\partial \varvec{K}}{\partial \rho _{e}} \varvec{u}_{e}\right) . \end{aligned}$$(20)Here, an adjoint variable \(\lambda \) is defined as:
$$\begin{aligned} \varvec{\lambda }^{\mathrm {T}}=\frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \sigma _{e}^{v M}}\left( \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e}}\right) ^{T}\varvec{D_{0}BK^{1}}. \end{aligned}$$(21)Thus, we obtain the adjoint equations:
$$\begin{aligned} \varvec{K\lambda }=\frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \sigma _{e}^{v M}}\varvec{B^{\mathrm {T}}D_{0}^{\mathrm {T}}}\frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e}}. \end{aligned}$$(22)Then, by solving Eq. (22), we obtain the adjoint variable \(\lambda \) which is inserted into Eq. (20) so that a final gradient of \(\tilde{\sigma }_{\text{ norm } }^{P N}\) can be expressed as,
$$\begin{aligned} \frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \rho _{e}}=\frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \sigma _{e}^{v M}}\left( \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e}}\right) ^{T} q \rho _{e}^{q1} \varvec{D}_{0} \varvec{B} \varvec{u}_{e}\rho _{e}^{q} \varvec{\lambda }^{\mathrm {T}} \frac{\partial \varvec{K}}{\partial \rho _{e}} \varvec{u}_{e}, \end{aligned}$$(23)where, the terms \(\partial \tilde{\sigma }_{\text{ norm } }^{P N}/\partial \sigma _{e}^{v M}\)and \(\partial \sigma _{e}^{v M}/\partial \sigma _{e}\) are determined by Eq. (13) and Eq. (14) (or Eq. (15)) respectively. And as we know that,
$$\begin{aligned} \frac{\partial \varvec{K}}{\partial \rho _{e}}=\omega \rho _{e}^{\omega 1}\bar{E}_{e}\varvec{K}^{0}. \end{aligned}$$(24)So we can substitute Eq. (24) into equation Eq. (23) to get
$$\begin{aligned} \frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \rho _{e}}=\frac{\partial \tilde{\sigma }_{\text{ norm } }^{P N}}{\partial \sigma _{e}^{v M}}\left( \frac{\partial \sigma _{e}^{v M}}{\partial \sigma _{e}}\right) ^{T} q \rho _{e}^{q1} \varvec{D}_{0} \varvec{B} \varvec{u}_{e}\omega \rho _{e}^{q+\omega 1} \varvec{\lambda }^{\mathrm {T}} \bar{E}_{e}\varvec{K}^{0} \varvec{u}_{e}. \end{aligned}$$(25)
Projectionbased ROM approaches
Onthefly ROM construction using PCA
For largescale topology optimization problems, the main computational workload stems from the numerical solution of the equilibrium equation at each iteration:
where, the computation of this highprecision fullfield solution involves the inversion of a highdimensional linear systems that can consist of up to millions or billions of degrees of freedom (DOF) [30]. Since the coefficient matrix \(\varvec{K}\) is typically illconditioned (due to the SIMP interpolation) and also has a large number of DOFs, traditional methods depending on iteration methods like PCG may still be inadequate to significantly reduce the computational cost.
To alleviate this solution process, the authors call on a previouslyproposed method called onthefly ROM construction using PCA [28]. The gist of this approach is mapping the displacement field solution of the largescale problem Eq. (26) to a lowdimensional space spanned by an appropriately obtained orthonormal basis \(\varvec{\Phi }\)(\(\varvec{\Phi }^{\mathrm {T}}\varvec{\Phi }=\varvec{\mathrm{I}}\)) that is constructed onthefly and updated by implementing PCA for a set of stored solution snapshots obtained during the previous iterations. Here, we briefly present the salient features of the approach.
Given a snapshot matrix consisting of \(N_{b}\) displacement solutions at previous \(N_{b}\) successive iterations,
by zeromean processing for matrix \(\varvec{U}\), we obtain its centered version \(\varvec{\bar{U}}\),
then performing singular value decomposition (SVD) on the centered matrix \(\varvec{\bar{U}}\), we have,
the reduced basis \(\varvec{\Phi }\) is obtained by truncating the first \(M\ll N_{b}\) columns corresponding to the largest \(N_{b}\) singular values in matrix \(\varvec{\Psi }\) which is composed of \(N_{b}\) left singular vectors \(\varvec{\phi _{i}},i=1,\cdots ,N_{b}\),
usually, the value of M (i.e. the size of reduced basis \(\varvec{\phi }\)), is determined by following energy rule:
where, \(\kappa _{i}\) denotes the ith largest singular value of centered matrix \(\varvec{\bar{U}}\) and \(\varepsilon _{t r u n c}\) is a userdefined truncation error (in this paper 1%).
Now, by mapping the displacement field \(\varvec{u}\) on to the lowdimensional space spanned by the reduced basis \(\varvec{\Phi }\) constructed above, we have the following ROM expression,
Substituting the approximate solution \(\varvec{\tilde{u}}\) into Eq. (26) and then projecting the equations onto the basis, we get a reduced system with a much smaller dimensionality,
the high computational cost of solving fullscale system Eq. (26) may then be greatly reduced through a significantly less expensive solution of Eq. (33). Finally, a linear combination of projection coefficient \(\varvec{\alpha }\) as in Eq. (32) is used to recover the fullfiled solution.
The approximate accuracy of \(\varvec{\tilde{u}}\) is monitored during the optimization via the residual equilibrium error which is given by,
when the force residual of a certain optimization loop iteration (after at least \(N_{b}\) iterations have been completed so as to be able to obtain the basis) is lower than a prespecified threshold \(\hat{e}_{rb}\), we accept the reducedbasis solution in place of the fullfield solution. Once the force residual exceeds the tolerance \(\hat{e}_{rb}\), we are forced to recompute a fullfield solution of Eq. (26) by the direct method, and then use this new solution to replace the “oldest” stored displacement vector in current snapshot matrix. In order to reduce the storage requirements for large scale problems, recalculating PCA basis for a single snapshot update, the incremental PCA can be considered as shown in the reference [35]. In this way, the original basis is updated and improved using PCA for the next loop iteration, which forms the socalled onthefly construction and updating of the ROM.
Here two points have to be noted. Firstly, the construction of the snapshot matrix, requiring the solution of Nb linear systems, may be done by an iterative solver (see [28]), avoiding fullsize \(\varvec{K}\) construction. Secondly, the projection of the linear problem in Eq. (33) also does not require the assembly of the global stiffness matrix \(\varvec{K}\), as the reduced matrix \(\varvec{\Phi }^\mathrm{T}\varvec{K}\varvec{\Phi }\) and the RHS term \(\varvec{\Phi }^\mathrm{T}\varvec{K}\) may be assembled directly by projecting individual element contributions.
Multifidelity ROM construction using multigrid
Topology optimization with ROMbased reanalysis (as seen in “Onthefly ROM construction using PCA”) still suffers from a significant computational burden, as we need to repeatedly update the reduced basis to obtain a ”sufficiently good” prediction of the displacement field when the accuracy of the ROM is insufficient. The new snapshot is then treated as a fullfield solution calculated on a fine fixed FE mesh (i.e. singlefidelity), which should be effectively computed in some way. So, based on the above mentioned method, [26] proposed an approach of multifidelity ROM construction using the multigrid method, where the original equilibrium equations are solved on grids of various resolutions, and then quickly obtain a multifidelity snapshot solution for constructing and updating the reduced basis. Next, A typical ”V” cycle MG iteration of recursive form is given in Algorithm 1 as follows (\(\ell =1,2,\cdots ,n1\)):
In this paper, we set the level number \(n=2\) and \(\beta _{1}=\beta _{2}=3\) , i.e. a simple twogrid “V” cycle. And we choose the FE displacement solution obtained from the previous main optimization loop as the initial guess \(\varvec{u}_{\ell }\), details of the coarse grid operators \(\varvec{K}^{(\ell +1)}=(\varvec{P}^{\ell }_{\ell +1})^{\mathrm {T}}\varvec{K}^{\ell }\varvec{P}^{\ell }_{\ell +1}\) and prolongation operators can be seen in [24]. The smooth operators use the PCG method. Algorithm 1 starts from \(MG (\varvec{K}^{(1)}, \varvec{f}^{(1)},\varvec{u}^{(1)},1)\) , where \(\varvec{K}^{(1)}=\varvec{K},\varvec{f}^{(1)}=\varvec{f}\). For the sake of accuracy, we repeat the above “V” cycle loop twice (initial guess for the next loop is selected as the MG solution of the previous loop)
The algorithms for both approaches (introduced in “Projectionbased ROM approaches”) are combined in Algorithm 2, where SFROM stands for onthefly ROM construction using PCA using singlefidelity (SF) snapshots calculated on a fixed FE mesh, and MFROM for multifidelity ROM construction using multigrids where multifidelity (MF) snapshots are obtained by MG iteration. Fullorder model (FOM) represents the fullfield solution in Eq. (26) obtained using either the direct method (for SFROM) or the MG method (for MFROM).
Two improved strategies
AdapROM
Whether we use the SFROM or the MFROM, a pivotal ROM parameter, the force residual threshold \(\hat{e}_{rb}\) must always be predefined by users. Sometimes it’s hard to give an appropriate value of \(\hat{e}_{rb}\) as it clearly involves a tradeoff between calling the ROM solution and the FOM solution during the optimization procedure. On the one hand, if we use a smaller value, then the optimal objective may have better accuracy but would require more CPU time as the FOM would ostensibly be called more frequently, on the other hand, if we use a bigger value, then the optimal objective may have poorer accuracy but would require less CPU time as the ROM would tend to be called more frequently. Therefore, in this paper, we propose an adaptive selection strategy for the value of force residual threshold which is then chosen according to the relative error variation of objective function value during the iteration loop.
\(c_{i1}, c_{i2} \) are the objective function values at two consecutive iterations \({i1}_{th}\) and \({i2}_{th}\), here the relative erroris gradually decreasing because of the convergence behavior of the compliance minimization problem. Details of the strategy are summarized in the following Algorithm 3.
In this paper, we set \(\theta >1\) , so that the force residual threshold changes from a relatively smaller value towards a bigger value as the relative error \(e_{c}\) reduces. More specially, the adaptive selection of \(\hat{e}_{rb}\) is roughly divided into three stages: In the first stage, \(e_{c}\) is relatively higher and so the FOM rather than ROM is called on to maintain the stability of the optimization procedure. In the second stage, the variation of the objective function is less, so we begin using the ROM with a smaller value of \(\hat{e}_{rb}\) . Finally in the third stage, \(e_{c}\) is small enough (meaning that objective is sufficiently converged) therefore a larger value \(\hat{e}_{rb}\) of can be used, thus the ROM solution is more readily accepted. Note that the code in Algorithm 3 may be directly inserted between lines 7 and 8 in Algorithm 2 for obtaining a new version of ROM using adaptive parameter selection for the residual threshold.
BiROM
Recall that in “Introduction”, we have mentioned that stressconstrained topology optimization problems are generally nonselfadjoint, and will yield an additional adjoint equation (see (Eq. (22)) derived from sensitivity analysis of the stress constraint function, that needs to be solved. Taking advantage of the fact that the adjoint equation is of the same scale as the FE equilibrium equations, it would seem logical to apply the ROM idea given in Algorithm 2 to the adjoint equations, giving:
where, \(\Xi \) is the reduced basis, \(\mu \) represents the projection coefficients and \(\bar{\lambda }\) is the mean snapshot for the set of adjoint solutions. An important feature here is that the construction of the ROM for the adjoint equation and the equilibrium equations in this paper are completely independent, which means the snapshot number and residual threshold of the ROM for the adjoint equations could be completely different from those for the equilibrium equations.
Numerical tests
In this section, we first apply the two ROM methods that were introduced in “Projectionbased ROM approaches”: SFROM and MFROM to a 2D benchmark stressconstrained compliance minimization problem. Next, using MFROM, we demonstrate the effectiveness of the two improved strategies that were presented in “Two improved strategies”. In order to better understand the impact of the parameters associated with the stress constraints on optimal design, we use different values for the p norm factor p, the stress penalty factor q and the allowable maximum stress \(\hat{\sigma }\) for numerical experiments using a benchmark 3D Lshaped beam. Unless otherwise stated, the variables and geometric parameters are dimensionless for all test examples in this paper. Predefined parameters: Young’s modulus \(E_{0}=1\) for the solid material with a lower limit \(E_{\min }=10^{9}\) for void material, Poisson’s ratio \(\nu =0.3\). The penalty factor of stiffness \(\omega =3\), density filter \(r_{\min }=2.5\) and the allowable volume fraction \(\hat{v}_{f}=0.2\). Since the objective function (here compliance) is conveniently represented using a separable convex approximation by the Method of Moving Asymptotes (MMA), which is easily adapted to different types of topology optimization problems, we retain the MMA as the optimizer for iteration loop. The optimization iterations stop either when the convergence condition is satisfied or once the maximum allowable number of iterations is reached. Here, the convergence criterion is defined as follows:
where, \(\left\ \cdot \right\ _{2}\) denotes the binary norm of a vector. i denotes the current iteration step, and Tol is the allowable convergence error, in this paper, \(Tol=10^{4}\).
2D Lshaped beam
Consider the classical optimization problem of the 2D Lshaped beam [4, 5, 8, 10], the design domain and boundary conditions are illustrated in Fig. 1. The structure’s top face on the left side is fixed and an external load \(f=1\) is applied on the top right corner A. We use 16384 bilinear quadrilateral elements to discretize the design domain, each element having unit volume and thickness. To avoid stress concentration at the loading node A, the concentrated loadis evenly distributed over the 6 adjacent nodes between node A and B, as shown in Fig. 1. For this 2D case, we set the p norm factor \(p=8\), the stress penalty factor \(q=0.8\) and the allowable maximum stress. The maximum iteration number is set to 200. Note that for all test cases shown hereafter, the iterations were halted due to the maximum allowable number of optimization loop iterations having been attained.
Table 1 shows the optimal topology and corresponding stress distribution obtained using the reference method (without ROM), as well as the SFROM method and the MFROM method using a fixed snapshot number \(N_{b}\) and various values for the force residual threshold \(\hat{e}_{rb}\). Figures 2 and 3 compare the iteration histories for the convergence of the compliance and stress (von Mises stress \(\sigma ^{vM}_{\max }\) and Pnorm stress \(\sigma ^{PN}\)) between the SFROM and MFROM methods.
From Table 1 a macroscopic view leads us to the premature conclusion that the optimal topology using SFROM and MFROM seem basically consistent with that using the reference method; but on closer inspection more structural branches occur and the arc of reentry of the Lshaped beam is more distinct when using a bigger value of \(\hat{e}_{rb}\) . And it should be noted that for both SFROM and MFROM, stress concentration still exists at the location of the applied force. Figure 2 shows that the objective optimization is converged regardless of whether or not we use SFROM or MFROM. Figure 3 shows that stress constraints using both the SFROM and MFROM are active and gradually satisfied during the overall optimization procedure. Furthermore, due to the constraint violation shown in Fig. 3, the convergence history of the objective function is nonmonotonous as shown in Fig. 2.
The above design results are summarized in Table 2, where the relative error of the optimal compliance (\(c^{*}\)) characterizes the approximate accuracy of the objective function value using ROM,
where, \(c^{*}_{refe}\) and \(c^{*}_{rom}\) represent the optimal compliance obtained by using the reference method and the ROM method respectively.
From Table 2, as we increase the value of \(\hat{e}_{rb}\) , the CPU clock time using both SFROM and MFROM show a significant decrease compared to the reference method, which is easy to explain : the cheaper reducedbasis solution (ROM) is called more frequently, thus the computational efficiency of the overall optimization routine is improved. However, the optimal compliance using both ROM methods has a very poor accuracy if we use a larger value of the force residual threshold (\(\hat{e}_{rb}=0.5\)). This indicates that we must make a tradeoff between efficiency and accuracy. Furthermore, by comparing the performance of the MFROM with the SFROM, we find that MFROM can further drive down the computational cost with a minor loss of objective accuracy when using the same set of values of \(N_{b}\) and \(\hat{e}_{rb}\).
Next, we use the first improved strategy: adaptive parameter selection of the force residual threshold \(\hat{e}_{rb}\) to modify the MFROM method in “Projectionbased ROM approaches”. Some parameters need to be predefined: initial force residual threshold \(\hat{e}^{0}_{rb}=0.05\) and its scale factor \(\theta =10\), initial limit of objective relative error (see Eq. (32)) \(\hat{e}^{0}_{rb}=2\times 10^{3}\) and its decay factor \(\varsigma =10^{1}\) . The optimized design results are summarized in Table 3 and Fig. 4 shows the optimal topology using the MFROM and AdapROM as well as the reference method.
From Table 3, we see that topology optimization using AdapROM has a clear advantage in terms of accuracy compared to the MFROM method using a bigger force residual (\(\hat{e}_{rb}=0.5\)), while requiring less computational time compared to the reference method, as well as the MFROM method using a smaller \(\hat{e}_{rb}=0.05\) (as expected), which shows that this improved method allows a good compromise between accuracy and speed. From Fig. 4 we see that the optimal topology obtained using AdapROM is closer to that obtained using the reference method, compared to the optimal topology obtained using MFROM, which is again expected. Next we give the change history of relative error \(e_{c}\) generated by using AdapROM in Fig. 5a, which allows us to decide when to use different force residual thresholds. And Fig. 5b gives the evolutionary curve of the force residual \(e_{rb}\).
Then, for the same 2D benchmark stressconstrained topology optimization problem, we use another improved strategy BiROM to modify the MFROM method in “Projectionbased ROM approaches” . For the equilibrium equations (Eq. (23)), we set \(N_{b}=4\) and \(e_{rb}=0.1\), for adjoint equations (Eq. (21)), we set \(N_{b}=6\) and \(e_{rb}=0.05\) . The design results are summarized in Table 4 and Fig. 6 shows the optimal topology obtained using MFROM and BiROM as well as reference method.
From Table 4 we can see that BiROM is less time consuming compared to the MFROM and the accuracy of the optimized compliance is better. Figure 6 shows that the BiROM appears to yield a clearer optimal topology than the MFROM method.
Figure 7 shows the iteration history for the force residual \(e_{rb}\) of the equilibrium equations as well as the adjoint equations, using the BiROM method.
A conclusion may be directly drawn from Fig. 8 that for the BiROM, the ROM solution of the adjoint equations is more readily “acceptable” than that of the equilibrium equations, even for smaller values of \(e_{rb}\) . This is because the residual evolutionary curve of equilibrium equations frequently oscillated above and below the threshold line(red) while the residual evolutionary curve of equilibrium equations basically stays below the threshold line as the iteration progresses.
Finally, we combine the AdapROM and BiROM methods together (denoted by AdapBiROM) to further improve the MFROM method. Some parameters are predefined like before: initial limit of objective function relative error \(\hat{e}_{c}^{0}=2\times 10^{3}\) decay factor \(\varsigma =10^{1}\) , for the equilibrium equations: \(N_{b}=4\) , initial force residual threshold \(\hat{e}_{c}^{0}=0.05 \) with scale factor \(\theta =10\), for adjoint equations \(N_{b}=6\), initial force residual threshold \(\hat{e}_{c}^{0}=0.01 \) and its scale factor \(\theta =10\). The optimized design results are summarized in Table 5 as follows.
From Table 5 we can see, the combined strategy AdapBiROM shows better performance than any one of the individual strategies(AdapROM or BiROM) from a holistic perspective since this combined method can not only significantly reduce the computation time but also ensure a high accuracy of the value of objective function.
Discussion
The multifidelity reducedordermodel (MFROM) approach clearly enhances the performance of the topology optimization procedure with a superior reduction of computational effort and CPU time compared with singlefidelity reducedordermodel (SFROM) for all the test cases studied, noting that a small loss of accuracy of the objective function is expected when using MFROM. By using the first proposed improved strategy (AdapROM) of adaptively selecting the force residual threshold (\(\hat{e}_{rb}\)) in MFROM, we found a tradeoff can be made between optimization efficiency and objective accuracy. We also note that the second proposed improved strategy (BiROM) of applying MFROM method to both adjoint equations derived from sensitivity analysis of stress constraint function and equilibrium equations in FE analysis can reduce the CPU running time in a more significant manner. In addition, even better accuracy of objective function can be obtained compared with the original MFROM method (for this 2D case at least), this may be because using a ROM for the adjoint equations corrects the convergence of the objective function. Finally, we combined both strategies and this can obtain better optimized results because there is a significant improvement in efficiency with a higher accuracy of approximation for the objective function.
3D Lshaped beam
In the previous section, we investigated the application of reanalysis using ROM in stressconstrained topology optimization through a 2D numerical example. In this section, we apply the previously described ROM methods to the 3D compliance minimization problem of the Lshaped beam. To better understand the influence of the stress constraint on the optimization results, we then consider making an in depth analysis of some of the parameters associated with the stress constraint based on the AdapBiROM method. The Lshaped beam is shown in Fig. 8, where the structure’s top surface is fixed and a vertically downward load \(f=1\) is applied along the top right side.
We use standard hexahedral elements to discretize the design domain with each element having unit volume and thickness. The maximum number of iterations is set to 300.
ROM methods on 3D Lshaped beam
Here, we set \(L=80\) and \(W=50\), thus the design domain is discretized by a total of 32768 elements. 5 ROM methods were tested for this 3D case, The corresponding design results are given in Table 6.
From Table 6 we see that the combined AdapBiROM method behaves well both as far as computational time saving as well as final objective accuracy are concerned, as expected, in the 3D largescale test case. Next, we will use this method as the ROM approach of choice to conduct a parameter study.
Parametric study
For this, we set \(L=50\) and \(W=6\) in Fig. 8, thus the design domain is discretized by a total of 9600 elements. Some parameters are predefined as follows: initial limit of objective relative error \(\hat{e}^{0}_{c}=5\times 10^{3}\) and its decay factor \(\varsigma =10^{2}\), for equilibrium equations \(N_{b}=4\):,initial force residual threshold \(\hat{e}^{0}_{c}=0.04\) and its scale factor \(\theta =20\), for adjoint equations \(N_{b}=6\):, initial force residual threshold \(\hat{e}^{0}_{c}=0.01\) and its scale factor \(\theta =50\).
Influence of p norm factor p
Here, we vary the p norm factor from 2 to 30, and while fixing the stress penalty factor at \(q=0.8\) and the allowable maximum stress at \(\hat{\sigma }\). Table 7 gives the design results.
It can be seen from Table 7 that the CPU runtime trend for both the reference method as well as the combined AdapBiROM method is not monotonic. More computation time is spent when using a smaller p value (like 2 and 4) while less time is spent when using a larger p value (like 20 and 30) for these two methods. However, both methods still have some differences in terms of the changing trend of the CPU runtime, where the CPU time of the reference method goes down while that of the AdapBiROM method goes up, when we vary the p value from 6 to 8.
Interestingly, we find that the optimal compliance obtained using both methods has the same trend of first dropping and then increasing as the value of p increases, which means that we can likely obtain the smallest optimal compliance (meaning the “stiffest” possible structure) by using a midrange value for p. In general, to better balance CPU time and structural performance, the p value should neither be too large nor too small.
Figures 9, 10 and 11 show the optimal topology and stress iterative history as well as the volume fraction iteration history for different values of the Pnorm p norm factor with the AdapBiROM method.
We see from Fig. 9 that the optimal topologies obtained using different values of p based on AdapBiROM method are visually different when using \(p=4\) and \(p=6\) (or \(p=12\) and \(p=20\)).
From Fig. 10, we can see that the stress value during the entire procedure satisfy its constraint limit progressively faster with a larger value of p. Meanwhile, it seems that the larger the value of p, the smaller the value of the final maximum von Mises stress \(\sigma _{\max }^{VM}\). For \(p=20\) and \(p=30\), the curves are below the stress limit within 50 iterations.
Fig. 11 shows that the volume fraction during the iterations can rapidly, and in a stable manner, satisfy its respective constraint limiting value, provided \(p > 2\).
Next, we give a comparison of the compliance (objective function) iteration history using different values of p based on AdapBiROM method in Fig. 12 where it appears that the larger the p value, the faster the rate of convergence of the optimization.
Investigation of varying stress penalty factor q
We vary the stress penalty factor q while fixing the p norm factor \(p= 8\) and the allowable maximum stress at. Table 8 gives the design results.
It can be seen from Table 8 that the trends for CPU time and optimal compliance for both the reference method and the AdapBiROM method are exactly the same and not monotonic as the q value decreases. Therefore, the ROM retains the same impact of the stress penalty factor parameter as for the reference case. Interestingly, the CPU time has a general tendency to first increase and then decrease while the optimal compliance has the opposite tendency, implying a potential conflict between CPU time and optimal compliance for several q values. This means that q needs to be properly determined to better balance the computational efforts and structural performance.
Just like in “Influence of p norm factor p”, we give the optimal topology and stress iteration history as well as the volume fraction iteration history for different values of the stress penalty factor, using the AdapBiROM method, as shown in Figs. 13, 14 and 15, respectively.
From Fig. 13 we can see that the optimal topologies using different values of q based on AdapBiROM method are visually distinguishable from each other, which can be seen from the test case with \(q=0.5\) and \(q=0.8\).
From Fig. 14 we note that the stress constraint is not satisfied when using relatively smaller values of \(q (0.1  0.3)\) which means the stress penalization is not sufficient. In addition, using a larger value of q can cause the maximum von Mises stress to satisfy its constraint limiting value as soon as possible during the procedure. In the case of \(q=0.9\), the curves end up below the stress limit after about 25 iterations.
Figure 15 shows that the volume fraction during the iterations can rapidly and in a stable manner satisfy the constraint for all 5 different values of q tested here.
Next, we compare the compliance iteration histories using different values of q based on the AdapBiROM method in Fig. 16 where different convergence rates of optimization can be obtained by varying q, but no monotonicity is observed as q increases. It seems plausible that a midrange value of q would lead to a relative lower convergence rate as shown below.
Varying the allowable maximum stress
In this case, we vary the allowable maximum stress \(\hat{\sigma }\)while simultaneously fixing the p norm factor p at 8 and the stress penalty factor q at 0.8. Table 9 gives the design results.
From Table 9 we see that the trends for the CPU time are the same for both the reference as well as the AdapBiROM methods, first increasing and then decreasing as the \(\hat{\sigma }\) value increases. A similar trend is seen for the optimal compliance for both methods.
Just like in the previous investigations, we give the optimal topology and stress iteration history as well as the volume fraction iteration history for different values of the allowable maximum stress based on the AdapBiROM method, as shown in Figs. 17, 18 and 19, respectively.
From Fig. 17 we can see that the optimal topologies using different values of \(\hat{\sigma }\) based on the AdapBiROM method are clearly very different from each other. When using smaller values of \(\hat{\sigma }\) (\(\hat{\sigma }=0.15\) ,\(\hat{\sigma }=0.3\) ), the final design structural branches are discontinuous and in a “fractured” state which means that the optimized design has not yet converged sufficiently despite having completed maximum iterations. Interestingly, we find a clear curvature forming at the corner of the Lshaped beam by using these two smaller values of \(\hat{\sigma }\) . As for other values of \(\hat{\sigma }\) , the optimal topologies are also different from each other (see the case of \(\hat{\sigma }=0.45\) and \(\hat{\sigma }=0.65\) ).
From Fig. 18 we can see that the stress constraint is not satisfied in the case of the smallest value of \(\hat{\sigma }\) (\(\hat{\sigma }=0.15\) ). Also the maximum von Mises stress constraint is increasingly easier to satisfy during the procedure as \(\hat{\sigma }\) increases, but we note that an overtly large value of \(\hat{\sigma }\) could potentially render the stress constraint inactive (as seen in the case of \(\hat{\sigma }=0.65\) and \(\hat{\sigma }=0.75\) ).
From Fig. 19 we can see that the volume constraint is not satisfied for smaller values of \(\hat{\sigma }=0.15\) or \(\hat{\sigma }=0.3\) despite having been satisfied for larger values of \(\hat{\sigma }\).
Finally, we compare the compliance iteration history using different values of \(\hat{\sigma }\) and the AdapBiROM method in Fig. 20, where the compliance clearly has different convergence rate depending on the values of \(\hat{\sigma }\) and a relatively large value of \(\hat{\sigma }\) could potentially accelerate convergence.
Conclusions and perspectives
In this paper, we first presented two novel ROMbased Approximate Reanalysis approaches: onthefly ROM using Principal Components Analysis (SFROM) and multifidelity ROM using multigrid method (MFROM) and applied them to the nonselfadjoint stressconstrained topology optimization problem, and assessed their performance in terms of efficiency and reduction in computation time, using a 2D benchmark problem. Furthermore, we improved the second approach with two improved strategies: a socalled AdapROM method where the residual threshold of the equilibrium equations is adaptively selected according to the relative error of the objective function value during the iteration; and the socalled BiROM method where the ROM is simultaneously applied to both the equilibrium equations as well as the adjoint equations obtained from the sensitivity analysis of the stress constraint. The first improved strategy achieves a balance between efficiency and accuracy, while the second improved strategy can further reduce the computational effort needed. To amplify the effect of the ROM, we combined both strategies for this 2D numerical example showing a good balance between efficiency and accuracy.
We then tested various versions of the ROM methods in this paper through a 3D Lshaped beam. Then using the combined version of AdapROM and BiROM, we studied various parameters associated with the stress constraint, including the Pnorm factor, the stress penalty factor as well as the allowable maximum stress value, in order to better understand the influence of the stress constraint on the ROMbased optimization results. We showed that the aforementioned parameters have a significant effect on the final optimized results (efficiency, structural performance etc), and therefore a judicious selection of these key parameters is required.
Furthermore, from the point of view of storage, the amount of storage required for the proposed onthefly ROM approach is much smaller compared to that needed for the fullfield problem with finite element simulation calculation during the optimization process. The proposed method only needs to store a small dimension snapshot matrix of small dimensionality to obtain the reduced basis. The only thing that needs to be done sequentially is the onthefly updating of the reduced basis using the residual errors, in order to ensure the quality of approximation.
A logical extension of this work would focus on efficient largescale dynamic topology optimization. In addition, other nonselfadjoint problems besides the numerical examples presented in this paper need to be addressed.
Availability of data materials
The data sets and models used and/or analysed during the current study are available from the corresponding author on reasonable request.
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Acknowledgements
The first author expresses her sincere gratitude to the associate professor Kai Long at North China Electric Power University for his help in testing the codes in its initial stages.
Funding
This research study was supported by the National Natural Science Foundation of China (Grant No. 12032018, Grant No. 11620101002 and Grant No. 11972166) and the Natural Science Foundation of Shaanxi Province, China (Grant No. 2021JM043).
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MX, WZ developed the main idea of the two novel approaches and introduced JM, and DL to implement benchmark test case, analyze numerical results and prepare the concept manuscript. BR provided his feedback on the manuscript. All authors read and approved the final manuscript.
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Dr. Manyu Xiao, Associate professor, School of Mathematics and Statistics of Northwestern Polytechnical University, Xi’an, Shaanxi, People’s Republic of China. Mr. Jun Ma, Dongcheng Lu, Master students, School of Mathematics and Statistics of Northwestern Polytechnical University, Xi’an, Shaanxi, People’s Republic of China. Dr. Balaji Raghavan, Associate professor, Laboratoire de Génie Civil et Génie Mécanique EA 3913, Institut National des Sciences Appliquées de Rennes, Rennes, France. Prof. Weihong Zhang, Academician of the Chinese Academy of Sciences, State IJR Center of Aerospace Design and Additive Manufacturing, Northwestern Polytechnical University, Xi’an, 710072, People’s Republic of China.
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Xiao, M., Ma, J., Lu, D. et al. Stressconstrained topology optimization using approximate reanalysis with onthefly reduced order modeling. Adv. Model. and Simul. in Eng. Sci. 9, 17 (2022). https://doi.org/10.1186/s4032302200231x
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DOI: https://doi.org/10.1186/s4032302200231x