Dynamic analysis of grouped turbo blades using radial basis function

Dynamic analysis of grouped turbo blades using radial basis function

Eigenvalue problems of grouped turbo blades were numerically formulated using a radial basis function. This study investigated different boundary conditions, which accompany the radial basis function, for transforming partial differential equations of grouped turbo blades into a discrete eigenvalue...

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Bibliographic Details
Main Authors: Ming-Hung Hsu, Paul Juinn Bing Tan
Format: Article
Language:English
Published: SAGE Publishing 2015-06-01
Series:Advances in Mechanical Engineering
Online Access:https://doi.org/10.1177/1687814015582004
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spelling doaj-3e29ab75d70140d5b3c0c06f9dbe36702020-11-25T02:22:54ZengSAGE PublishingAdvances in Mechanical Engineering1687-81402015-06-01710.1177/168781401558200410.1177_1687814015582004Dynamic analysis of grouped turbo blades using radial basis functionMing-Hung HsuPaul Juinn Bing TanEigenvalue problems of grouped turbo blades were numerically formulated using a radial basis function. This study investigated different boundary conditions, which accompany the radial basis function, for transforming partial differential equations of grouped turbo blades into a discrete eigenvalue problem. The numerical results show the validity and efficiency of the radial basis function for solving this problem. The crack depth considerably affects the dynamic behavior of grouped turbo blades.https://doi.org/10.1177/1687814015582004
collection DOAJ
language English
format Article
sources DOAJ
author Ming-Hung Hsu
Paul Juinn Bing Tan
spellingShingle Ming-Hung Hsu
Paul Juinn Bing Tan
Dynamic analysis of grouped turbo blades using radial basis function
Advances in Mechanical Engineering
author_facet Ming-Hung Hsu
Paul Juinn Bing Tan
author_sort Ming-Hung Hsu
title Dynamic analysis of grouped turbo blades using radial basis function
title_short Dynamic analysis of grouped turbo blades using radial basis function
title_full Dynamic analysis of grouped turbo blades using radial basis function
title_fullStr Dynamic analysis of grouped turbo blades using radial basis function
title_full_unstemmed Dynamic analysis of grouped turbo blades using radial basis function
title_sort dynamic analysis of grouped turbo blades using radial basis function
publisher SAGE Publishing
series Advances in Mechanical Engineering
issn 1687-8140
publishDate 2015-06-01
description Eigenvalue problems of grouped turbo blades were numerically formulated using a radial basis function. This study investigated different boundary conditions, which accompany the radial basis function, for transforming partial differential equations of grouped turbo blades into a discrete eigenvalue problem. The numerical results show the validity and efficiency of the radial basis function for solving this problem. The crack depth considerably affects the dynamic behavior of grouped turbo blades.
url https://doi.org/10.1177/1687814015582004
work_keys_str_mv AT minghunghsu dynamicanalysisofgroupedturbobladesusingradialbasisfunction
AT pauljuinnbingtan dynamicanalysisofgroupedturbobladesusingradialbasisfunction
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