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contributor authorAli, Sazeed S.
contributor authorYadav, Vikas S.
contributor authorNouri, Behnam
contributor authorGhani, Abdulla
date accessioned2025-04-21T10:30:40Z
date available2025-04-21T10:30:40Z
date copyright12/23/2024 12:00:00 AM
date issued2024
identifier issn0742-4795
identifier othergtp_147_07_071004.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4306343
description abstractThe conventional iterative optimization of turbine blades using computer-aided engineering simulations is resource-intensive, with high costs and time demands, as well as significant challenges in computational requirements and data management. The three-dimensional (3D) simulation data generated from computational fluid dynamics (CFD) and finite element analysis (FEA) for various blade geometries can range from hundreds of gigabytes to multiple terabytes, complicating long-term storage and access. To address this, we propose a machine learning-based methodology for data reduction and prediction of 3D surface field data. Our approach involves developing a convolutional variational auto-encoder (VAE), consisting of an encoder and a decoder. The encoder compresses the input data into a representation of reduced dimensionality in a latent space, while the decoder reconstructs the data from this latent space back to its original form. This significantly reduces the amount of stored data, facilitating long-term use. Additionally, we train a fully connected feedforward multilayer perceptron (MLP) to map geometry parameters, which generate blade variations, to the latent space. By combining the MLP with the VAE's trained decoder, we create our proposed multilayer perceptron–variational auto-encoder (MLP–VAE) hybrid model capable of predicting surface field data for new, unseen blade geometries. The MLP–VAE generates latent representations and surface field results with high accuracy (>97%) and without additional computational costs, offering a highly efficient and scalable solution for turbine blade optimization.
publisherThe American Society of Mechanical Engineers (ASME)
titleHybrid Surrogate Modeling Approach for Data Reduction and Design Space Exploration of Turbine Blades
typeJournal Paper
journal volume147
journal issue7
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.4066998
journal fristpage71004-1
journal lastpage71004-11
page11
treeJournal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 007
contenttypeFulltext


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