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REVIEW 4 major objections 3 minor 161 references

Towards Automatic and Reliable Localized Model Order Reduction

T0 review · 4 major / 3 minor · reviewed 2026-08-14 · deepseek-v4-flash

Pith's one-line read The paper claims a complete localized model order reduction pipeline that makes resimulation after local geometry changes nearly independent of the unchanged global mesh.

desk verdict A solid, honest MOR thesis with rigorous localized error bounds and randomized training, but the certified-reliability claim is only demonstrated for coercive problems and the estimator constants are never actually computed. read the letter →

arxiv 1908.02074 v1 pith:QKMLCFAP submitted 2019-08-06 math.NA cs.NA

classification math.NAcs.NA MSC 65N3065N1565N55
keywords localizedmodelorderreductionreducedbasismethodaposteriorierrorestimationrandomizednumericallinearalgebratransferoperatorwirebasketspacedecompositiononlineenrichmentprintedcircuitboardsimulation
verification ladder T0 review T1 audit T2 compute T3 formal

The pith

A machine-rendered reading of the paper's core claim, the machinery that carries it, and where it could break.

The reading

The thesis assembles a localized model order reduction pipeline, named ArbiLoMod, for sequences of finite-element simulations in which only small, non-parametric parts of the geometry change between runs. Its central claim is that local training, local a posteriori error estimation, and local online enrichment can be combined so that after a local design edit only the reduced spaces in the changed region need to be recreated, and the global problem is then solved on a small reduced system. The paper further claims a new training algorithm: applying a randomized range finder to a transfer operator on each local patch produces reduced spaces that converge, with high probability, at essentially the singular value decay rate of that operator. If these claims hold, interactive workflows such as signal-integrity simulation of printed circuit boards could resimulate local modifications without re-solving the global high-dimensional problem from scratch.

What carries the argument

The wirebasket space decomposition is the backbone: each degree of freedom is assigned to a coarse mesh entity and extended to neighboring cells by solving the homogeneous equation, giving a direct-sum splitting of the global space into local subspaces. The transfer operator $T$ maps boundary or coupling data on a local training domain to the local solution within it; the randomized range finder approximates the image of its linear part, and the training a priori estimate $\|u-\tilde u\|/\|u\| \le \sqrt{\gamma/\alpha}\, \sqrt{\bar J J^*}\,\max_i \|(1-P_{\tilde V_i})T_i^l\|\,\|P_{S_i}\|$ turns the global error into a bound on local projection errors. The partition-of-unity dual norm localization bounds the residual norm by $\sqrt{\bar J}\,c_{pu,\tilde V}\,(\sum_i \|R_\mu(\tilde u_\mu)\|_{V_i'}^2)^{1/2}$, which makes the error estimator computable from local solves.

What would settle it

For the 2D Maxwell or Olimex A64 example, compute an independently certified lower bound for the inf-sup constant; if the localized error estimator then fails to be an upper bound on the true reduction error, or if the bound cannot be computed without a global solve, the reliability claim fails.

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Extended reading notes

Core claim

ArbiLoMod decomposes the global finite-element space via a wirebasket decomposition: reduced subspaces are attached to coarse vertices, edges, faces, and cells, with basis functions extended into neighboring cells by solving homogeneous local problems. The initial reduced spaces are built by local trainings (random boundary data on a patch around each interface) and by local greedy algorithms; a partition-of-unity based a posteriori error estimator bounds the residual dual norm by the sum (or root-sum-square) of local residual norms, with constants that can be computed or bounded, and an online enrichment loop adds the steepest residual components until the estimated error falls below tolerance. The principal new analytical claims are a probabilistic a priori bound for the randomized training, showing the generated local spaces are nearly as good as the optimal singular-value spaces of the transfer operator, and exponential convergence of the proposed online enrichment algorithms. All ingredients are demonstrated on thermal-channel, two-dimensional Maxwell, and a 65-million-degree-of-freedom printed-circuit-board example; for the inf-sup stable Maxwell problems the author reports that a certified inf-sup lower bound is not provided.

Load-bearing premise

The entire certified error bound rests on having a global lower bound for the coercivity constant (or the inf-sup constant) of the bilinear form, and the thesis computes such a bound only for simple heat-conduction examples, not for the inf-sup stable Maxwell or PCB cases that motivate the work.

Editorial extensions

If this is right

  • After a localized geometry change, only reduced spaces whose training domains intersect the change need to be regenerated; the rest of the offline data can be reused.
  • The localized a posteriori estimator gives a rigorous upper bound on the reduction error with computable constants in coercive problems, and it can steer where to enrich.
  • The randomized training algorithm replaces the user-chosen number of random samples with an adaptive choice, and its convergence rate is tied to the singular-value decay of the transfer operator.
  • The online enrichment loop converges exponentially and can even start from empty local bases, so it provides a fallback when initial training is insufficient.

Reading between the lines

Editorial extensions of the paper, not claims the author makes directly.

  • The missing certified inf-sup lower bound for the Maxwell and PCB examples is the one gap between the proven reliability statement and the stated target application; a localized or randomized inf-sup estimator would close it.
  • Because the training a priori estimate is independent of the number of local subdomains, the method should scale to very large domain decompositions; a three-dimensional PCB example with thousands of subdomains would be a natural stress test.
  • The same randomized range finder could be warm-started with reduced bases from previous geometries, potentially making the reuse after local changes even cheaper than rebuilding from scratch.
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Editorial analysis

A structured set of objections, weighed in public.

Desk editor's note, referee report, and a circularity audit.

Referee Report

4 major / 3 minor

Summary. The manuscript is a PhD thesis proposing ArbiLoMod, a localized model order reduction methodology for sequences of PDE simulations with arbitrary local geometry modifications. It develops a wirebasket space decomposition with local training, a localized residual-based a posteriori error estimator via dual norm localization, randomized range finder training algorithms with probabilistic a priori convergence bounds, and online enrichment algorithms. The main claims are that ArbiLoMod delivers a complete localized pipeline, that the localized error estimator is certified with computable constants, and that randomized training converges nearly as fast as the singular value decay of the transfer operator. Numerical experiments cover heat conduction, a 2D Maxwell problem, and a large PCB example, with reproduction scripts.

Significance. The strongest contributions are the abstract localized training configuration with the transfer-operator formulation and the randomized range finder analysis in Chapter 5, including a probabilistic a posteriori norm estimator and an a priori convergence theorem; these are rigorous and are supported by numerical experiments on the Olimex A64 example. The numerically stable offline/online splitting for the reduced basis error estimator in Section 4.5 is a useful practical contribution, and the emphasis on reproducible source code is commendable. If the certification gap described below is resolved, the localized a posteriori estimator would be a significant step toward localized model order reduction for engineering applications. As it stands, however, the certified reliability claim is not established for the targeted Maxwell/PCB application, which is the central weakness of the manuscript.

major comments (4)
  1. [Sections 4.2–4.3, Corollary 4.2.4; Sections 2.6.4 and 3.6.2] The localized error estimator is certified only for coercive problems. Corollary 4.2.4 applies Proposition 4.2.3 to the standard error bound Δ(ũμ) = 1/αμ ‖Rμ(ũμ)‖, which requires a computable lower bound on the coercivity constant αμ. The time-harmonic Maxwell problem in H(curl) (Section 2.6.4) is inf-sup stable but not coercive, and the text states that a lower bound for the inf-sup constant is not computed. Therefore the reliable/certified status claimed in the abstract and in design goal (5) of Section 3.1 is not demonstrated for the main target application; Section 3.6.2 indeed runs the 2D Maxwell experiment without the a posteriori error estimator. The authors should either present an inf-sup lower bound for the Maxwell setting (or its 2D normal-magnetic reduction) or explicitly restrict the certification claim to coercive problems.
  2. [Section 3.6.1, Figure 3.11] The sole numerical demonstration of the localized estimator in the Thermal Channels example is plotted for αμ = cpu,~V = 1. This means the constants whose computability is claimed in the abstract are not actually computed or bounded by their certified estimates in the experiment, and the effectivity of the estimator is not shown. Since the main selling point of Corollary 4.2.4 over the standard global estimator is a localized, computable, certified bound, the demonstration should report the computed or estimated constants, or at least compare the estimator with a certified lower bound using the bounds from Propositions 4.3.2 and 4.3.3.
  3. [Section 5.1, Proposition 5.1.3, Eq. (5.16)] The a priori training estimate rests on the assumption T_a^i ∈ ~V_i (Eq. 5.16), i.e., the affine part of each transfer operator is contained in the reduced local space. In the parameterized ArbiLoMod pipeline, the training algorithms only include snapshots for a finite set Ξ (e.g., Algorithm 3.3, and the randomized range finder in Section 5.2 targets the linear part T_l^i), so this hypothesis is not guaranteed for parameters outside the training set. The text should either prove that the construction enforces Eq. (5.16) for all parameters, or restate the theorem with an additional affine-part/residual term and explain how training controls it.
  4. [Section 3.6.2, Figures 3.16–3.17] For the inf-sup stable Maxwell example, the reduced Galerkin problem is observed to become unstable at certain basis sizes, with the reduced inf-sup constant dropping and the maximum error jumping at a basis size of about 900. The thesis acknowledges this and defers stable Petrov-Galerkin reduction to future work in Section 3.7. This is an honest limitation, but it further means that the method as presented cannot yet be certified for the target inf-sup stable application, and this restriction should be stated prominently in the abstract and conclusions rather than only in the experiment section.
minor comments (3)
  1. [Section 1.4.4 and Bibliography] There are copy-editing problems, for example the sentence fragment in Section 1.4.4 ('CMS Component Mode Synthesis (CMS) component mode synthesis (CMS) introduced in a [Hurty(1965),Bampton and Craig(1968)]') and bibliography entries with 'doi: n/a'; these should be cleaned up before submission.
  2. [Section 3.6.1, Figure 3.11] The text says the factor cpu,~V is 'neglected' while the caption says 'Plotted for αμ = cpu,~V = 1'; the terminology should be unified so that the reader knows whether the plotted quantity is an upper bound, a lower bound, or a heuristic indicator.
  3. [Section 4.3, Proposition 4.3.2] In the proof, the estimate is first obtained with H_i in the denominator and then stated with H = min_i H_i; a one-line clarification that H ≤ H_i justifies the uniform bound would improve readability.

Circularity Check

0 steps flagged · score 0.0 of 10

Derivation chain is self-contained; no circularity found.

full rationale

The paper's main derived results are self-contained in the sense that their statements do not coincide by definition with their inputs. The ArbiLoMod training pipeline is analyzed in Proposition 5.1.3, where the reduction error is bounded by the projection error of the transfer operator under the explicit decomposition assumption u = Σ_i T_i P_{S_i} u|_{ω*_i} (Definition 5.1.1, Eq. 5.3); this is an assumption of the framework, not the conclusion of the theorem, and the subsequent randomized range finder bounds that projection error by a standard RandNLA estimate involving the singular values of the operator (Section 5.2). Similarly, the localized a posteriori error estimator in Corollary 4.2.4 is derived from the residual dual norm and the localized stability constants c_{i,~V} and c_{pu,~V}; these constants are defined directly in terms of the reduced space and the space decomposition, and no fitted parameter is renamed as a prediction. The only caveats are explicit limitations: Section 2.6.4 states "we cannot in general estimate the inf-sup constant from below. Obtaining a lower bound for the inf-sup constant is a challenging task which we omit", and Section 3.6.2 applies ArbiLoMod to the 2D Maxwell problem "without ... a posteriori error estimator", so the certified-reliability claim is not demonstrated for the target inf-sup-stable application; Figure 3.11 is plotted for αµ = cpu,~V = 1, so the constants' computability is not numerically demonstrated. These are correctness or validation gaps, not circular reductions. The thesis also cites the author's own prior journal articles (e.g., Buhr and Smetana 2018, Buhr et al. 2017a), but the corresponding analyses are reproduced in the thesis itself and the cited publications are peer-reviewed, so the self-citations are not load-bearing in the derivation chain.

Assumptions & free parameters 4 free parameters · 6 assumptions · 0 invented entities

No fitted physical parameters appear in the derivations; the free parameters are algorithmic tolerances that control basis size. The axioms are the structural assumptions of the space decomposition, the affine parameter dependence, availability of stability constants (a known weak point), and conditions used in the training and localization estimates. No new physical entities are introduced.

free parameters (4)
  • M (number of random samples in heuristic training)
    User-chosen in Algorithm 3.3; the improved randomized range finder in Chapter 5 replaces it with an adaptive selection depending on a prescribed accuracy and failure probability.
  • epsilon_train (training tolerance)
    Stopping criterion for the snapshot greedy in local face space training; set to 1e-4 or 1e-5 in experiments, affects basis size but not the mathematical claims.
  • epsilon_greedy (greedy tolerance)
    Stopping criterion for local cell space greedy; set to 1e-3 to 1e-7 in experiments.
  • r (enrichment fraction)
    Doerfler-like fraction in the enrichment loop, set to 0.5 in experiments.
assumptions (6)
  • domain assumption The localizing space decomposition satisfies sum V_i = V and sum P_V_i(phi) = phi for all phi in V.
    Definition 2.4.1; the wirebasket decomposition is designed to satisfy it, but it is a structural requirement for the localized error estimates and training a priori bound.
  • domain assumption The bilinear form has an affine parameter dependence.
    Section 2.3, Eq (2.17); standard in reduced basis methods; used for offline/online splitting.
  • ad hoc to paper A computable lower bound for the coercivity constant alpha_LB (or inf-sup lower bound) is available.
    Used in residual-based estimators (Eq (3.21), Eq (4.1)). The thesis admits such bounds are not available for general problems, in particular for the inf-sup stable Maxwell case (Section 2.6.4).
  • ad hoc to paper The affine part T_a^i of each transfer operator is contained in the reduced space ~V_i (Eq 5.16).
    Needed for the training a priori estimate Prop 5.1.3; if not enforced, the bound has an extra term. The training algorithm must include the right-hand-side response to satisfy this.
  • domain assumption The partition of unity functions rho_i are contained in the reduced space ~V (Prop 4.3.3).
    Used to obtain an H-independent bound on the localization constant; in ArbiLoMod this is fulfilled because vertex spaces (codim 2) are kept full-dimensional.
  • standard math Random coefficient vectors produce inner products with a Gaussian distribution with variance bounded by the extreme eigenvalues of the inner product matrix (Lemma 5.2.1).
    This is a standard property of Gaussian random vectors and is used for the probabilistic norm estimator.

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Cite this review

Pith. "Pith review of Towards Automatic and Reliable Localized Model Order Reduction." pith.science (2026). https://pith.science/paper/QKMLCFAP

@misc{pith2026190802074,
  author       = {Pith},
  title        = {Pith review of: Towards Automatic and Reliable Localized Model Order Reduction},
  year         = {2026},
  howpublished = {\url{https://pith.science/paper/QKMLCFAP}},
  note         = {Machine review of arXiv:1908.02074}
}
read the original abstract

Finite element based simulation of phenomena governed by partial differential equations is a standard tool in many engineering workflows today. However, the simulation of complex geometries is computationally expensive. Many engineering workflows require multiple simulations with small, non parametric changes in between. The use of localized model order reduction for subsequent simulations of geometries with localized changes is very promising. It produces lots of computational tasks with little dependencies and thus parallelizes well. Furthermore, the possibility to reuse intermediary results in the subsequent simulations can lead to large computational savings. In this thesis, we investigate different aspects of localized model order reduction and propose various improvements. A simulation methodology named ArbiLoMod, comprising a localized training, a localized a posteriori error estimator and an enrichment procedure is proposed. A new localized a posteriori error estimator with computable constants is presented and analyzed. A new training algorithm which is based on a transfer operator is derived. It can be shown to converge nearly as fast as the singular value decay of this operator. The transfer operator's spectrum is observed to decay fast in electromagnetic simulations in printed circuit boards. New online enrichment algorithms are proposed. All results are supported by numerical experiments, for which the source code for reproduction is provided.

Figures

Figures reproduced from arXiv: 1908.02074 by the authors.

Figure 1.1
Figure 1.1. DDR memory channel on a printed circuit board subject to local modification of conductive tracks (own photo, manipulated with GIMP). 1 [PITH_FULL_IMAGE:figures/full_fig_p021_1_1.png] view at source ↗
Figure 2.1
Figure 2.1. Visualization of Nédélec ansatz functions (edge elements) for one triangle (reproduc￾tion: Appendix A.1). where the restriction to the boundary is to be understood in the sense of traces. The space H(curl, Ω) is defined as usual as H(curl, Ω) := n ϕ ∈ [PITH_FULL_IMAGE:figures/full_fig_p040_2_1.png] view at source ↗
Figure 2.2
Figure 2.2. Geometry of Thermal Block Example: Four blocks of constant, but parameterized, heat conductivity. 2.7.1. Thermal Block Example The first numerical example we denote by Thermal Block Example. It is a simple parametric example which is often used in introductory texts on parameterized model order reduction (for example in [Patera and Rozza(2007)] or [Haasdonk(2017)]). We solve the problem in Definition 2.1.1 with the … view at source ↗
Figures from the paper (48 more)
Figure 2.3
Figure 2.3. Figure 2.3: High-dimensional solution of Equation (2.73) in Thermal Block Example for µ = (0.1, 1.0, 0.4, 0.1). (reproduction: Appendix A.2) [PITH_FULL_IMAGE:figures/full_fig_p044_2_3.png]
Figure 2.4
Figure 2.4. Figure 2.4: First structure in sequence of simulated structures in Thermal Channels Example. Unit square with high and low conductivity regions. White: constant conductivity region (σ = 1), black: parameterized high conductivity region (σµ = 1 + µ). Homogeneous Neumann boundarie…
Figure 2.5
Figure 2.5. Figure 2.5: Sequence of structures simulated in Thermal Channels Example along with solutions for one parameter value. Localized changes in the geometry cause global changes in the solution. (reproduction: Appendix A.3) 25 [PITH_FULL_IMAGE:figures/full_fig_p045_2_5.png]
Figure 2.6
Figure 2.6. Figure 2.6: Geometries simulated in 2D Maxwell Example. Black area is not part of the domain and treated as Dirichlet zero boundary. Note that the change is topology changing [PITH_FULL_IMAGE:figures/full_fig_p047_2_6.png]
Figure 2.7
Figure 2.7. Figure 2.7: Example solutions for 2D Maxwell Example for ω = 2π·186 MHz, ω = 2π·561 MHz and ω = 2π · 1 GHz for the first and second geometry. Plotted is |Re(E)|. (reproduction: Appendix A.4) boundary condition. Note that the geometry is slightly asymmetric intentionally, to prod…
Figure 2.8
Figure 2.8. Figure 2.8: Front and perspective view of Olimex A64 Example. 2.7.4. Olimex A64 Example The fourth example is the Olimex A64 Example. Here we solve the problem in Definition 2.1.1 with the bilinear form and the linear form defined as in Equation (2.58) and the space V defined in…
Figure 2.9
Figure 2.9. Figure 2.9: Back and detail view of Olimex A64 Example. In the right picture, the meandering traces between the CPU (top) and the RAM (left) are visible [PITH_FULL_IMAGE:figures/full_fig_p049_2_9.png]
Figure 2.10
Figure 2.10. Figure 2.10: Meshed detail of Olimex A64 Example. Metal parts, modeled as Dirichlet boundaries, are shown in red. A staircase approximation of the geometry is used. air copper prepreg copper FR4 copper prepreg copper FR4 copper prepreg copper air 350 µm 35 µm 127 µm 35 µm 500 µm…
Figure 2.11
Figure 2.11. Figure 2.11: Stackup of Olimex A64 Example: Six layers of metal with insulating layers in between. Data provided by Olimex in private communication. 29 [PITH_FULL_IMAGE:figures/full_fig_p049_2_11.png]
Figure 3.1
Figure 3.1. Figure 3.1: Main components of localized model order reduction • Localized training • Localized a posteriori error estimation • Localized online enrichment Those parts form a global loop, as visualized in [PITH_FULL_IMAGE:figures/full_fig_p052_3_1.png]
Figure 3.2
Figure 3.2. Figure 3.2: Overview of ArbiLoMod. Generation of initial reduced interface spaces by training and of reduced volume spaces by greedy basis generation is subject of Section 3.3 and Chapter 5. Convergence is assessed with the localized a posteriori error estimator presented in Cha…
Figure 3.3
Figure 3.3. Figure 3.3: Visualization of basic spaces V basic i and their extension spaces for Q1 ansatz functions (one DoF per mesh node). Definition 3.2.1 (Basic subspaces). For each element i ∈ {1, . . . , NE } we define a basic subspace V basic i of Vh as: V basic i := span n ψ ∈ B [PI…
Figure 3.4
Figure 3.4. Figure 3.4: Visualization of some example elements of the local subspaces V wb i for inhomogeneous coefficients. The structure in the solution results from variations in the heat conduction coefficient. (a) Value 1 in V basic i (b) Linear in V basic j , j ∈ Υ1 (c) Solving in V b…
Figure 3.5
Figure 3.5. Figure 3.5: Extend operator is executed in two steps for spaces V wb i , i ∈ Υ2. Mesh and spaces as depicted in [PITH_FULL_IMAGE:figures/full_fig_p056_3_5.png]
Figure 3.6
Figure 3.6. Figure 3.6: Visualization of spaces for a codim 1 coarse mesh entity. Basic space V basic i , training space, and the coupling space of training space for Q1 ansatz functions (one DoF per mesh node). 3.3.2. Local Training for Basis Construction of Reduced Face Spaces To generate…
Figure 3.7
Figure 3.7. Figure 3.7: Data dependencies in ArbiLoMod: Before online enrichment, it is possible to compute all reduced basis function having support on a domain (ω nol 5 here) using only local information about the domain and its surrounding domains. 43 [PITH_FULL_IMAGE:figures/full_fig_p…
Figure 3.8
Figure 3.8. Figure 3.8: Maximum relative H1 -error on training set Ξ in dependence of tolerances in codim 1 training and codim 0 greedy for Thermal Channels Example. Online enrichment disabled. (reproduction: Appendix A.6) work can be distributed on many nodes. Afterwards, only reduced repr…
Figure 3.9
Figure 3.9. Figure 3.9: Relative error over iteration with and without basis reuse for after geometry change for Thermal Channels Example. With codim 1 training. Convergence criterion: kRµ(ueµ)kVh 0 < 10−4 , greedy tolerance: εgreedy = 10−5 . See also [PITH_FULL_IMAGE:figures/full_fig_p065…
Figure 3.10
Figure 3.10. Figure 3.10: Relative H1 error over iterations with and without basis reuse for after geometry change for Thermal Channels Example. Without codim 1 training. Convergence criterion: kRµ(ueµ)kV 0 h < 10−4 , greedy tolerance: εgreedy = 10−5 . See also [PITH_FULL_IMAGE:figures/full…
Figure 3.11
Figure 3.11. Figure 3.11: Error estimators ∆rel(ueµ) and ∆ g loc,rel(ueµ) over iterations, compared to the relative error for Thermal Channels Example. Plotted for αµ = c pu,Ve = 1. Simulation performed with a convergence criterion of kRµ(ueµ)kV 0 h < 10−6 , a training tolerance of εtrain = …
Figure 3.12
Figure 3.12. Figure 3.12: Distribution of local basis sizes after initial training for Thermal Channels Exam￾ple. Relative reduction error at this configuration: 1.3 · 10−3 . (reproduction: Ap￾pendix A.11) computing environment. Especially when the solution has to be calculated at multiple p…
Figure 3.13
Figure 3.13. Figure 3.13: inf-sup and continuity constant of bilinear form for 2D Maxwell Example. Linear and logarithmic. (reproduction: Appendix A.12) 0 20 40 60 80 100 10−15 10−7 101 basis size max rel. projection error geometry 1 geometry 2 [PITH_FULL_IMAGE:figures/full_fig_p069_3_13.png]
Figure 3.14
Figure 3.14. Figure 3.14: Error when approximating the solution set for all µ ∈ Ξ with an n-dimensional basis obtained by greedy approximation of this set. This is an upper bound for the Kolmogorov n-width. (2D Maxwell Example) (reproduction: Appendix A.13) excitation [PITH_FULL_IMAGE:figur…
Figure 3.15
Figure 3.15. Figure 3.15: Domain decomposition used for 2D Maxwell Example. 49 [PITH_FULL_IMAGE:figures/full_fig_p069_3_15.png]
Figure 3.16
Figure 3.16. Figure 3.16: Maximum error when solving 2D Maxwell Example with a localized basis, generated by global solves. (reproduction: Appendix A.14) 0 1,000 2,000 10−9 10−6 10−3 100 basis size maximum relative error 0 1,000 2,000 10−4 10−3 10−2 10−1 100 basis size eβ 170 MHz 340 MHz 700…
Figure 3.17
Figure 3.17. Figure 3.17: Comparison of maximum error over all frequencies with inf-sup constant of reduced system at selected frequencies for geometry 1. Basis generated by global solves. Increased error and reduced inf-sup constant at basis size of ca. 900 (2D Maxwell Example). (reproducti…
Figure 3.18
Figure 3.18. Figure 3.18: Maximum error over all frequencies for both geometries of 2D Maxwell Example. Basis generated by global solves vs. basis generated by local training. (reproduction: Appendix A.16) Dahmen et al.(2014)] to the localized setting is not straightforward. Properties of Tr…
Figure 3.19
Figure 3.19. Figure 3.19: Impact of geometry change of 2D Maxwell Example: 5 domains contain changes, 14 domain spaces and 20 interface spaces have to be regenerated. geo 1: geo 2 [PITH_FULL_IMAGE:figures/full_fig_p072_3_19.png]
Figure 3.20
Figure 3.20. Figure 3.20: Basis size distribution in 2D Maxwell Example. (reproduction: Appendix A.11) have to be regenerated. All other bases can be reused, which results in large computational savings compared to a simulation from scratch. However, the Galerkin projection leads to an unsta…
Figure 4.1
Figure 4.1. Figure 4.1: Evaluation of proposed offline/online splitting: maximum relative reduction errors and estimated reduction errors (H1 -norm) for numerical example Thermal Block Example. (reproduction: Appendix A.18) space Ve is constructed from the linear span of solutions to Defini…
Figure 5.1
Figure 5.1. Figure 5.1: Geometry of Rangefinder Example 1 and Rangefinder Example 2 Analytic interface problem To analyze the behavior of the proposed algorithm, we first apply it to an analytic problem where the singular values of the transfer operator are known. We refer to this numerical…
Figure 5.2
Figure 5.2. Figure 5.2: Comparison of optimal basis functions with the basis functions generated by Algo￾rithm 5.1 for Rangefinder Example 1 . Basis functions are normalized to an L 2 (Γin) norm of one. (reproduction: Appendix A.19) 0 5 10 100 10−5 10−10 10−15 basis size n [PITH_FULL_IMAGE…
Figure 5.3
Figure 5.3. Figure 5.3: Projection error supξ∈S\{0} infζ∈Ren kTξ−ζkR kξkS = [PITH_FULL_IMAGE:figures/full_fig_p105_5_3.png]
Figure 5.4
Figure 5.4. Figure 5.4: Projection error supξ∈S\{0} infζ∈Ren kTξ−ζkR kξkS = [PITH_FULL_IMAGE:figures/full_fig_p107_5_4.png]
Figure 5.5
Figure 5.5. Figure 5.5: h dependency in Rangefinder Example 1 ; Statistics over 10,000 samples. (reproduc￾tion: Appendix A.23) 0 5 10 15 20 10−15 10−10 10−5 100 i σi+1 k = 0 k = 10 k = 20 k = 30 k = 40 0 5 10 15 20 0 20 10− 40 15 10−10 10−5 100 i κ σi+1 [PITH_FULL_IMAGE:figures/full_fig_p1…
Figure 5.6
Figure 5.6. Figure 5.6: Singular value decay for Rangefinder Example 2 . The red line at i = k/π in the right plot marks the observed length of the plateau. (reproduction: Appendix A.24) Γout and the boundary conditions are the same as in Section 5.3, only the operator A differs and is defi…
Figure 5.7
Figure 5.7. Figure 5.7: Projection error supξ∈S\{0} infζ∈Ren kTξ−ζkR kξkS = [PITH_FULL_IMAGE:figures/full_fig_p109_5_7.png]
Figure 5.8
Figure 5.8. Figure 5.8: Projection error supξ∈S\{0} infζ∈Ren kTξ−ζkR kξkS = [PITH_FULL_IMAGE:figures/full_fig_p109_5_8.png]
Figure 5.9
Figure 5.9. Figure 5.9: Domain decomposition used for Olimex A64 Example with 40 × 28 domains. For each domain ωi (e.g. ω816, yellow) we introduce an oversampling domain ω ∗ i (e.g. ω ∗ 816, green) [PITH_FULL_IMAGE:figures/full_fig_p110_5_9.png]
Figure 5.10
Figure 5.10. Figure 5.10: Example randomized solution in oversampling domain of ω816 of Olimex A64 Example (approx. 350.000 unknowns). For simplicity, we use the euclidean norm of the coefficient vectors in V basic 816 and compare with the singular values of the matrix of T l 816. In [PITH_…
Figure 5.11
Figure 5.11. Figure 5.11: Singular value decay of T816 and decay of randomized norm estimator for Olimex A64 Example. (reproduction: Appendix A.27) 815 820 825 830 835 840 845 850 855 0 200 400 600 domain time/s assembly factorization testvector generation basis generation [PITH_FULL_IMAGE:…
Figure 5.12
Figure 5.12. Figure 5.12: Runtimes for randomized range finder on Olimex A64 Example. (reproduction: Appendix A.27) 92 [PITH_FULL_IMAGE:figures/full_fig_p112_5_12.png]
Figure 6.1
Figure 6.1. Figure 6.1: Geometry of Thermal Channels Variant. Left: Coefficient field σ. White is 1, black is 105 . Middle: right hand side q. Black is −105 , gray is 0, white is 105 . Right: reference solution u. (reproduction: Appendix A.28) . . . . . . . . [PITH_FULL_IMAGE:figures/full…
Figure 6.2
Figure 6.2. Figure 6.2: Overlapping domain decomposition ωi (green and blue) constructed from 2×2 patches of non-overlapping domain decomposition (red) for Thermal Channels Variant. a variant of the Thermal Channels Example but driven by a right hand side instead of inhomoge￾neous boundary …
Figure 6.3
Figure 6.3. Figure 6.3: Decay of relative energy error during iteration for Thermal Channels Variant (zoom). (reproduction: Appendix A.29) 0 100 200 300 400 500 600 10−9 10−6 10−3 100 [PITH_FULL_IMAGE:figures/full_fig_p122_6_3.png]
Figure 6.4
Figure 6.4. Figure 6.4: Decay of relative energy error during iteration. (reproduction: Appendix A.29) 102 [PITH_FULL_IMAGE:figures/full_fig_p122_6_4.png]
Figure 6.5
Figure 6.5. Figure 6.5: Convergence of online enrichment in Thermal Channels Variant. 1 would be conver￾gence within one iteration, 0 would be stagnation. (reproduction: Appendix A.29) 0 100 200 300 400 500 600 100 103 106 numerical noise Iteration n equation (6.6) equation (6.7) equation (…
Figure 6.6
Figure 6.6. Figure 6.6: Sharpness of inequalities in Algorithm 6.1: For equation (6.6),  kuen − uk 2 a − kR(uen)k 2 O0 k  /  kuen+1 − uk 2 a  is plotted. For equation (6.7),  kR(uen)k 2 V 0 k  /  1 NVi PNVi i=1 kR(uen)k 2 V 0 k  is plotted. For equation (6.8),  c pu,Ve 2 PNVi i=1 k…

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