{"created":"2023-06-20T15:07:58.556067+00:00","id":37355,"links":{},"metadata":{"_buckets":{"deposit":"9591ef83-85fe-4b6d-bc5f-a35186a03222"},"_deposit":{"created_by":1,"id":"37355","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37355"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037355","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480323","480322"],"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 caused by crossflow disturbances"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"269","bibliographicPageStart":"265","bibliographicVolumeNumber":"41","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 24-26 Jun. 1998 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 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"圧縮性境界層を計算するナビエ・ストークスコード、擾乱の空間増幅を計算する線形PSE(Parabolized Stability Equations)コード、および増幅率を積分するN値法コードから成る境界層遷移予測システムを開発した。そしてこのシステムを、後退円柱上の圧縮性境界層の遷移が、Creelらが実験で観察したのと同様の幅方向の波長を持つ横流れ擾乱によって引き起こされる場合に適用した。このシステムによって、遷移開始の付着線からの角度間隔は32〜35度であることを予測した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A prediction system for boundary layer transition is developed which consists of the Navier-Stokes code computing a compressible boundary layer, the linear PSE (Parabolized Stability Equations) code computing the spatial growth of a disturbance, and the N-factor code integrating the growth rate. The system is applied to the case that the transition of the compressible boundary layer on a swept cylinder is caused by cross flow disturbances which have the same spanwise wavelength as observed in the experiment of Creel et al. It is predicted by the system that the angular distance from the attachment line for the transition onset is 32 deg to 35 deg.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958041","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-41","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":"nalsp0041041.pdf","filesize":[{"value":"353.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041041.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37355/files/nalsp0041041.pdf"},"version_id":"5c2def8d-ad63-466b-a21e-7f9e3667db9c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"横流れ擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移予測システム","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスコード","subitem_subject_scheme":"Other"},{"subitem_subject":"線形PSEコード","subitem_subject_scheme":"Other"},{"subitem_subject":"N値法コード","subitem_subject_scheme":"Other"},{"subitem_subject":"後退円柱","subitem_subject_scheme":"Other"},{"subitem_subject":"圧縮性境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"線形安定解析","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":"空間増幅","subitem_subject_scheme":"Other"},{"subitem_subject":"遷移開始位置","subitem_subject_scheme":"Other"},{"subitem_subject":"放物型安定方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速輸送機","subitem_subject_scheme":"Other"},{"subitem_subject":"後退翼","subitem_subject_scheme":"Other"},{"subitem_subject":"crossflow disturbance prediction system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boudary layer transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear PSE code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"N factor code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swept cylinder","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible boundary layer","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear stability analysis","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":"spatial growth","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transition onset location","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"parabolized stability equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"sweptback wing","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 paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"横流れ擾乱に起因する境界層遷移の予測","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"横流れ擾乱に起因する境界層遷移の予測"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37355","relation_version_is_last":true,"title":["横流れ擾乱に起因する境界層遷移の予測"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:21:05.509056+00:00"}