MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER

The centrifugal compressor is a prevalent type of turbo machinery with various applications. Among its components, the impeller plays a crucial role. Enhancing the performance of the centrifugal compressor impeller can trigger a cascading effect on the overall system performance. Currently, impeller...

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Main Author: Ikbar Syahputra, Reyhan
Format: Final Project
Language:Indonesia
Online Access:https://digilib.itb.ac.id/gdl/view/77145
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Institution: Institut Teknologi Bandung
Language: Indonesia
id id-itb.:77145
spelling id-itb.:771452023-08-22T15:37:21ZMULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER Ikbar Syahputra, Reyhan Indonesia Final Project centrifugal compressor, multi-objective optimization, surrogate model, CFD, genetic algorithm. INSTITUT TEKNOLOGI BANDUNG https://digilib.itb.ac.id/gdl/view/77145 The centrifugal compressor is a prevalent type of turbo machinery with various applications. Among its components, the impeller plays a crucial role. Enhancing the performance of the centrifugal compressor impeller can trigger a cascading effect on the overall system performance. Currently, impeller designs for centrifugal compressors are often developed using both theoretical and empirical calculations. However, the created designs can still be further optimized due to design methods being unable to determine specific design variables. This research focuses on multi-objective optimization of centrifugal compressor impeller design. Four design variables are selected from the control points of a third-degree Bezier curve. The optimization aims to maximize the pressure ratio and isentropic efficiency concurrently. The Non-Dominated Sorting Genetic Algorithm II (NSGA-II) is employed for this optimization. The genetic algorithm utilizes a surrogate model as a fitness function, constructed through Latin hypercube sampling of centrifugal compressor impeller performance evaluated using Computational Fluid Dynamics (CFD) simulations. Three optimal designs are obtained, each surpassing the initial design. Under design conditions, the efficiencies of Design A, Design B, Design C, and the initial design are 91.61%, 93.34%, 93.63%, and 90.30%, respectively. Meanwhile, the pressure ratios for Design A, Design B, Design C, and the initial design are 1.862, 1.855, 1.840, and 1.792, respectively. This indicates the dominance of the optimal designs over the initial design, without mutual domination among the optimal designs. text
institution Institut Teknologi Bandung
building Institut Teknologi Bandung Library
continent Asia
country Indonesia
Indonesia
content_provider Institut Teknologi Bandung
collection Digital ITB
language Indonesia
description The centrifugal compressor is a prevalent type of turbo machinery with various applications. Among its components, the impeller plays a crucial role. Enhancing the performance of the centrifugal compressor impeller can trigger a cascading effect on the overall system performance. Currently, impeller designs for centrifugal compressors are often developed using both theoretical and empirical calculations. However, the created designs can still be further optimized due to design methods being unable to determine specific design variables. This research focuses on multi-objective optimization of centrifugal compressor impeller design. Four design variables are selected from the control points of a third-degree Bezier curve. The optimization aims to maximize the pressure ratio and isentropic efficiency concurrently. The Non-Dominated Sorting Genetic Algorithm II (NSGA-II) is employed for this optimization. The genetic algorithm utilizes a surrogate model as a fitness function, constructed through Latin hypercube sampling of centrifugal compressor impeller performance evaluated using Computational Fluid Dynamics (CFD) simulations. Three optimal designs are obtained, each surpassing the initial design. Under design conditions, the efficiencies of Design A, Design B, Design C, and the initial design are 91.61%, 93.34%, 93.63%, and 90.30%, respectively. Meanwhile, the pressure ratios for Design A, Design B, Design C, and the initial design are 1.862, 1.855, 1.840, and 1.792, respectively. This indicates the dominance of the optimal designs over the initial design, without mutual domination among the optimal designs.
format Final Project
author Ikbar Syahputra, Reyhan
spellingShingle Ikbar Syahputra, Reyhan
MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
author_facet Ikbar Syahputra, Reyhan
author_sort Ikbar Syahputra, Reyhan
title MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
title_short MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
title_full MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
title_fullStr MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
title_full_unstemmed MULTIOBJECTIVE OPTIMIZATION DESIGN OF A CENTRIFUGAL COMPRESSOR IMPELLER
title_sort multiobjective optimization design of a centrifugal compressor impeller
url https://digilib.itb.ac.id/gdl/view/77145
_version_ 1822995217277517824