{"created":"2023-06-20T15:07:48.189507+00:00","id":37162,"links":{},"metadata":{"_buckets":{"deposit":"0eee055c-d9bf-435b-8b03-3b226b5706ed"},"_deposit":{"created_by":1,"id":"37162","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37162"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037162","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["479230","479231"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Prediction of boundary-layer transition on a swept cylinder"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1998-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"232","bibliographicPageStart":"229","bibliographicVolumeNumber":"37","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 12-13 Jun. 1997 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"境界層遷移を予測するシステムを開発した。本システムはナビエ・ストークスシミュレーション、線形安定解析およびe(exp N)法の3段階で構成される。本システムを無限後退円柱の付着線に沿った圧縮性境界層に適用した。異なる解を有する2つのタイプの格子により、円柱周りの格子を構成した。システム検証のため、これら格子で得た結果を各段階ごとに比較して、検証した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A system for prediction of boundary-layer transition is developed. The system consists of three stages, which are the Navier-Stokes simulation, linear stability analysis and e(exp N) method. The system is applied to the compressible boundary layer along the attachment line of an infinite swept cylinder. Two types of grids that have different resolutions are generated around the cylinder. The results obtained with these grids are compared at each stage to validate the system.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001433036","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-37","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野村, 聡幸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nomura, Toshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0037036.pdf","filesize":[{"value":"411.7 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0037036.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37162/files/nalsp0037036.pdf"},"version_id":"8e950ce2-7ade-495e-b6f3-d05bdcbb9b35"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"無限後退円柱","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"予測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスシミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"線形安定解析","subitem_subject_scheme":"Other"},{"subitem_subject":"付着線","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性境界層流","subitem_subject_scheme":"Other"},{"subitem_subject":"格子構成","subitem_subject_scheme":"Other"},{"subitem_subject":"シミュレーションコード検証","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移開始点","subitem_subject_scheme":"Other"},{"subitem_subject":"速度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"温度分布","subitem_subject_scheme":"Other"},{"subitem_subject":"Tollmien-Schlichting波","subitem_subject_scheme":"Other"},{"subitem_subject":"擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"infinite swept cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"prediction system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear stability analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"attachment line","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible boundary layer flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"grid generation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"simulation code validation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition starting point","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"velocity distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"temperature distribution","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Tollmien Schlichting wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"disturbance","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"jpn"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference 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