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非定常熱伝導場における形状同定問題の解法
http://hdl.handle.net/2237/7266
http://hdl.handle.net/2237/7266c3804c01-a743-421d-856b-86fd8827b39f
名前 / ファイル | ライセンス | アクション |
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JSME-B66-227.pdf (869.3 kB)
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Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2007-01-17 | |||||
タイトル | ||||||
タイトル | 非定常熱伝導場における形状同定問題の解法 | |||||
言語 | ja | |||||
その他のタイトル | ||||||
その他のタイトル | Solution to Shape Identification Problem of Unsteady Heat-Conduction Fields | |||||
言語 | en | |||||
著者 |
片峯, 英次
× 片峯, 英次× Katamine, Eiji× 畔上, 秀幸× Azegami, Hideyuki× 松浦, 易広× Matsuura, Yasuhiro |
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アクセス権 | ||||||
アクセス権 | open access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_abf2 | |||||
権利 | ||||||
言語 | ja | |||||
権利情報 | 日本機械学会 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Inverse Problem | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Optimum Design | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Numerical Analysis | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Unsteady Heat-Conduction | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Finite-Element Method | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Domain Optimization | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Shape Identification | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | Traction Method | |||||
抄録 | ||||||
内容記述 | This paper presents a numerical analysis method for shape determination problems of unsteady heat-conduction fields in which time-histories of temperature distributions on prescribed subboundaries or time-histories of gradient distributions of temperature in prescribed subdomains have prescribed distributions.The square error integrals between the actual distributions and the prescribed distributions on the prescribed subboundaries or in the prescribed subdomains during the specified period of time are used as objective functionals.Reshaping is accomplished by the traction method that was proposed as a solution to shape optimization problems of domains in which boundary value problems are defined.The shape gradient functions of these shape determination problems are derived theoretically using the Lagrange multiplier method and the formulation of material derivative.The time-histories of temperature distributions are evaluated using the finite element method for space integral and the Crank-Nicolson method for time integral.Numerical analyses of nozzle and coolant flow passage in wing are demonstrated to confirm the validity of this presented method. | |||||
言語 | en | |||||
内容記述タイプ | Abstract | |||||
出版者 | ||||||
言語 | ja | |||||
出版者 | 日本機械学会 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプresource | http://purl.org/coar/resource_type/c_6501 | |||||
タイプ | journal article | |||||
出版タイプ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
ISSN | ||||||
収録物識別子タイプ | PISSN | |||||
収録物識別子 | 03875016 | |||||
書誌情報 |
ja : 日本機械学会論文集 B編 巻 66, 号 641, p. 227-234, 発行日 2000-01 |
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フォーマット | ||||||
application/pdf | ||||||
著者版フラグ | ||||||
値 | publisher | |||||
URI | ||||||
識別子 | http://hdl.handle.net/2237/7266 | |||||
識別子タイプ | HDL |