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          <dc:title xml:lang="ja">重畳格子の概念を用いた非構造移動はめ込み型格子法(流体工学,流体機械)</dc:title>
          <jpcoar:creator>
            <jpcoar:creatorName xml:lang="ja">山川, 勝史</jpcoar:creatorName>
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          <jpcoar:creator>
            <jpcoar:creatorName xml:lang="ja">松野, 謙一</jpcoar:creatorName>
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          <dc:rights xml:lang="ja">本文データは学協会の許諾に基づきCiNiiから複製したものである</dc:rights>
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            <jpcoar:rightsHolderName xml:lang="ja">社団法人日本機械学会</jpcoar:rightsHolderName>
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          <jpcoar:subject xml:lang="en" subjectScheme="Other">Computational Fluid Dynamics</jpcoar:subject>
          <jpcoar:subject xml:lang="en" subjectScheme="Other">Compressible Flow</jpcoar:subject>
          <jpcoar:subject xml:lang="en" subjectScheme="Other">Unsteady Flow</jpcoar:subject>
          <jpcoar:subject xml:lang="en" subjectScheme="Other">Unstructured Mesh</jpcoar:subject>
          <jpcoar:subject xml:lang="en" subjectScheme="Other">Overset Grid</jpcoar:subject>
          <jpcoar:subject xml:lang="en" subjectScheme="Other">Moving Boundary Problem</jpcoar:subject>
          <datacite:description xml:lang="en" descriptionType="Abstract">From a point of view of grid generation, an overset grid generation method is suitable for a flow around moving complicated-shaped body. The overset grid method treats two grid-types which are a main-grid placed on all over the flow field and a sub-grid placed around the body. However it is difficult to satisfy a physical conservation law since the overset grid method interpolates the value between the main-grid and the sub-grid. To assure the conservation law on the overlapped region, we propose a new method that the overset grid method is combined to the unstructured moving grid finite volume method. In this method the sub-grid and the main-grid are joined by the unstructured grid. The feature of the method is that a control volume on which a space-time unified domain is adopted, and the method assures the geometric conservation law too even if the sub-grid moves and deforms. The method is applied to a problem such that complicated-shaped body flies in supersonic flow.</datacite:description>
          <datacite:description xml:lang="ja" descriptionType="Other">日本機械学会論文集(Ｂ編), 73巻, 734号, pp. 2070-2076, 20071025</datacite:description>
          <datacite:description xml:lang="en" descriptionType="Other">Submitted by 附属図書館 KIT-Repository (dspace-admin@jim.kit.ac.jp) on 2010-04-20T03:25:01Z No. of bitstreams: 1 110006419416.pdf: 1047937 bytes, checksum: ea94a7593b0e4402e28f9d13ee0bfaf4 (MD5)</datacite:description>
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          <dc:publisher xml:lang="ja">社団法人日本機械学会</dc:publisher>
          <datacite:date dateType="Issued">2007-10-25</datacite:date>
          <dc:language>jpn</dc:language>
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          <jpcoar:sourceTitle xml:lang="ja">日本機械学会論文集(Ｂ編)</jpcoar:sourceTitle>
          <jpcoar:volume>73</jpcoar:volume>
          <jpcoar:issue>734</jpcoar:issue>
          <jpcoar:pageStart>2070</jpcoar:pageStart>
          <jpcoar:pageEnd>2076</jpcoar:pageEnd>
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