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標(biāo)題: Titlebook: Evolutionary and Deterministic Methods for Design Optimization and Control With Applications to Indu; Esther Andrés-Pérez,Leo M. González, [打印本頁]

作者: raff淫雨霏霏    時(shí)間: 2025-3-21 19:56
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書目名稱Evolutionary and Deterministic Methods for Design Optimization and Control With Applications to Indu讀者反饋學(xué)科排名





作者: 巨頭    時(shí)間: 2025-3-21 20:24
Adjoint Shape Optimisation Using Model Boundary Representationed to define the geometry of a model is often integral to the efficiency of the design. However, it is not always possible to access these parameters due to the closed-source, non-standardized nature of most CAD software. A sensible choice, is to use standard CAD files which have an open format, in
作者: Inveterate    時(shí)間: 2025-3-22 02:46

作者: cardiovascular    時(shí)間: 2025-3-22 06:44

作者: 行業(yè)    時(shí)間: 2025-3-22 11:26
Node-Based Adjoint Surface Optimization of U-Bend Duct for?Pressure Loss Reduction gas turbines. The optimization technique proposed in the present work is based on the continuous adjoint shape method and is implemented in the OpenFOAM open-source framework. The calculated gradients of the objective function are linked to a node-based constrained morphing routine, allowing the mo
作者: Evolve    時(shí)間: 2025-3-22 15:29
Finite Transformation Rigid Motion Mesh Morphert each optimization cycle. Morphing has its share of challenges, namely to maintain high mesh quality (avoid distorted elements and tangles) even during extreme deformations. In this work, the Finite Transformation Rigid Motion Mesh Morpher (FT–R3M) is presented, an improved version of the Rigid Mot
作者: Evolve    時(shí)間: 2025-3-22 19:31

作者: guardianship    時(shí)間: 2025-3-23 00:06

作者: 船員    時(shí)間: 2025-3-23 04:07

作者: CYN    時(shí)間: 2025-3-23 06:08
A Comparative Evaluation of Surrogate Models for Transonic Wing Shape Optimizationing, Radial Basis Function Network (RBFN) and Proper Orthogonal Decomposition in combination with RBFNs (POD+RBFN) are employed as fitness function evaluators within the framework of evolutionary algorithms (EAs). The surrogate-assisted optimization consists of initializing the surrogate with space-
作者: LAY    時(shí)間: 2025-3-23 11:26
Study of the Influence of the Initial a Priori Training Dataset Size in the Efficiency and Convergenods is nowadays an attractive research field, as can be observed from the increasing number of scientific publications during the last years. Surrogate-based global optimization methods have demonstrated a huge potential to reduce the actual number of CFD runs, and therefore drastically speed-up the
作者: Debrief    時(shí)間: 2025-3-23 15:19
Garteur AD/AG-52: Surrogate-Based Global Optimization Methods in Preliminary Aerodynamic DesignAeronautical Research and Technology in Europe” and is a multinational organization that performs high quality, collaborative, precompetitive research in the field of aeronautics to improve technological competence of the European Aerospace Industry. The aim of the AG52 group was to make an evaluati
作者: CON    時(shí)間: 2025-3-23 21:08

作者: recede    時(shí)間: 2025-3-23 23:37

作者: 慢跑    時(shí)間: 2025-3-24 05:36
CFD Based Design Optimization of a Cabinet Nitrogen Generatornal Fluid Dynamics (CFD) based optimization could significantly improve the cooling efficiency of the critical parts of the components to ensure their performance and reliability. This work presents the CFD surrogate based optimization of the forced cooling of two reciprocating compressors located i
作者: NADIR    時(shí)間: 2025-3-24 07:37

作者: 進(jìn)步    時(shí)間: 2025-3-24 11:37
Evolutionary and Deterministic Methods for Design Optimization and Control With Applications to Indu
作者: 高談闊論    時(shí)間: 2025-3-24 17:11

作者: textile    時(shí)間: 2025-3-24 22:55
A Comparative Study of Two Different CAD-Based Mesh Deformation Methods for Structural Shape Optimizhe mesh deformation with an adjoint structural solver enables gradient computations of structural constraints with respect to CAD design parameters. To compare the robustness of the two mesh deformation methods, a CAD-based structural shape optimization using each method was performed.
作者: 軟弱    時(shí)間: 2025-3-25 03:14
Finite Transformation Rigid Motion Mesh Morpherthe internal nodes of the mesh (volume mesh), by keeping the motion of its parts (referred to as stencils) as–rigid–as–possible. It is an optimization–based method, which means that the interior nodes of the computational mesh are displaced to minimize a distortion metric, namely the deformation ene
作者: 真繁榮    時(shí)間: 2025-3-25 06:43
The Unsteady Continuous Adjoint Method Assisted by the Proper Generalized Decomposition Methodthis paper it that, apart from the standard PGD method, an incremental variant, running simultaneously with the time integration of unsteady primal equation(s) is proposed and tested. For the purpose of demonstration, three optimization problems based on different physical problems (unsteady heat co
作者: 休息    時(shí)間: 2025-3-25 11:17

作者: 無效    時(shí)間: 2025-3-25 11:58
Study of the Influence of the Initial a Priori Training Dataset Size in the Efficiency and Convergenique focused on optimization called the Intelligent Estimation Search with Sequential Learning (IES-SL). Several number of training points have been fixed to check the convergence, the accuracy and the objective function reached by the method.
作者: jabber    時(shí)間: 2025-3-25 19:46
Surrogate-Based Shape Optimization of the ERCOFTAC Centrifugal Pump Impellerc efficiency, while keeping the total pressure rise prescribed to the design condition, in order to find the optimal impeller design. The whole optimization chain is designed for running in HPC environment with open-source software, i.e. OpenFOAM for CFD simulation, Dakota for the optimization and S
作者: 鍍金    時(shí)間: 2025-3-25 21:42
CFD Based Design Optimization of a Cabinet Nitrogen Generator computational model to reduce the time and resources required. The combination of the ANN model with a multi start-gradient based algorithm optimized the position of compressors and cooling fans to minimize the average temperature on the critical parts. A set of new enclosure designs were found wit
作者: 完成才能戰(zhàn)勝    時(shí)間: 2025-3-26 03:18
Delaunay-Based Global Optimization in?Nonconvex Domains Defined by Hidden Constraintss modeled using an artificially-generated uncertainty function built on the framework of Delaunay triangulation. This work extends the Delaunay-based optimization algorithm with nonconvex constraints, dubbed .-DOGS(.), and extends this approach to estimate the feasible domain with binary oracle call
作者: Bombast    時(shí)間: 2025-3-26 04:45
Book 2019cation and optimization, multidisciplinary design optimization, applications of game theory to industrial optimization problems, applications in structural and civil engineering optimum design and surrogate models based optimization methodsin aerodynamic design..
作者: Obverse    時(shí)間: 2025-3-26 10:19
New Trends in Geometric Function Theory,orithm. At every optimization iteration a new profile is constructed using B-splines and the grid is rebuilt by elliptic grid generation. The gradients used for the optimization are obtained via a novel approach in which both the CAD kernel and grid generation are differentiated using Algorithmic Di
作者: 癡呆    時(shí)間: 2025-3-26 13:11
The Genesis of Modeling in Kindergartenhe mesh deformation with an adjoint structural solver enables gradient computations of structural constraints with respect to CAD design parameters. To compare the robustness of the two mesh deformation methods, a CAD-based structural shape optimization using each method was performed.
作者: Spina-Bifida    時(shí)間: 2025-3-26 17:21

作者: carbohydrate    時(shí)間: 2025-3-26 23:20

作者: 逗留    時(shí)間: 2025-3-27 03:55

作者: 祖先    時(shí)間: 2025-3-27 08:44

作者: 圖畫文字    時(shí)間: 2025-3-27 11:15

作者: 竊喜    時(shí)間: 2025-3-27 14:46

作者: Irrepressible    時(shí)間: 2025-3-27 19:57

作者: jaunty    時(shí)間: 2025-3-28 01:16

作者: 走調(diào)    時(shí)間: 2025-3-28 05:35

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作者: ATP861    時(shí)間: 2025-3-28 13:31

作者: Palpate    時(shí)間: 2025-3-28 17:36
https://doi.org/10.1007/978-3-642-25640-0ed to define the geometry of a model is often integral to the efficiency of the design. However, it is not always possible to access these parameters due to the closed-source, non-standardized nature of most CAD software. A sensible choice, is to use standard CAD files which have an open format, in
作者: Licentious    時(shí)間: 2025-3-28 20:17

作者: Trabeculoplasty    時(shí)間: 2025-3-28 23:47

作者: 遺傳學(xué)    時(shí)間: 2025-3-29 03:20
,Exploring Meinong’s jungle and beyond, gas turbines. The optimization technique proposed in the present work is based on the continuous adjoint shape method and is implemented in the OpenFOAM open-source framework. The calculated gradients of the objective function are linked to a node-based constrained morphing routine, allowing the mo
作者: 裝勇敢地做    時(shí)間: 2025-3-29 08:52

作者: CERE    時(shí)間: 2025-3-29 15:17

作者: 主動(dòng)    時(shí)間: 2025-3-29 16:23

作者: 發(fā)展    時(shí)間: 2025-3-29 20:51

作者: deactivate    時(shí)間: 2025-3-30 03:32

作者: GOUGE    時(shí)間: 2025-3-30 04:15
https://doi.org/10.1007/978-981-97-4962-1ods is nowadays an attractive research field, as can be observed from the increasing number of scientific publications during the last years. Surrogate-based global optimization methods have demonstrated a huge potential to reduce the actual number of CFD runs, and therefore drastically speed-up the
作者: 你不公正    時(shí)間: 2025-3-30 10:21
Exploring New Roles for LibrariansAeronautical Research and Technology in Europe” and is a multinational organization that performs high quality, collaborative, precompetitive research in the field of aeronautics to improve technological competence of the European Aerospace Industry. The aim of the AG52 group was to make an evaluati
作者: 免除責(zé)任    時(shí)間: 2025-3-30 12:26
William O’Brien,Andreas Wagner,Julia K. Dayonsists of two phases. In the first phase the compressor limits due to surge and choke are identified and approximated by utilizing methods of support vector machine (SVM). These limit lines are refined within an iterative, distance-based approach. Subsequently, in the second phase the three-dimensi
作者: 初學(xué)者    時(shí)間: 2025-3-30 17:07
https://doi.org/10.1007/978-3-319-98273-1rking at the design conditions. The aim of this paper is to investigate the potentialities offered by surrogate-based optimization techniques in centrifugal pump impeller shape optimization, to obtain a robust and fast algorithm for performance improvement. The geometry chosen for validating the pro
作者: 多節(jié)    時(shí)間: 2025-3-30 23:21

作者: Connotation    時(shí)間: 2025-3-31 01:15
Creativity Theory and Action in Educationions (a.k.a. hidden constraints). Both the objective function and the feasible domain are defined within a known rectangular domain. The objective function might be nonconvex, computationally expensive, and without analytic expression. Moreover, the feasible domain boundaries are not explicitly defi
作者: Projection    時(shí)間: 2025-3-31 07:18
978-3-030-07887-4Springer International Publishing AG, part of Springer Nature 2019
作者: 歌曲    時(shí)間: 2025-3-31 11:54
Evolutionary and Deterministic Methods for Design Optimization and Control With Applications to Indu978-3-319-89890-2Series ISSN 1871-3033 Series E-ISSN 2543-0203
作者: THROB    時(shí)間: 2025-3-31 16:29

作者: gorgeous    時(shí)間: 2025-3-31 17:40





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