{"created":"2023-06-20T15:07:27.374070+00:00","id":36829,"links":{},"metadata":{"_buckets":{"deposit":"688f237e-1063-48cf-90d2-ce3609a854cb"},"_deposit":{"created_by":1,"id":"36829","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"36829"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00036829","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["425068","425066","425063","425064","425065","425067"],"item_5_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"圧縮性層流制御の実験的および数値的研究"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"90","bibliographicPageStart":"81","bibliographicVolumeNumber":"31","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"境界層安定性について超音速風洞試験および数値解析を行った。風洞試験は後退翼モデルについて行った。境界層遷移位置をいくつかの迎え角で観測し、境界層吸気による層流域の拡大も観測した。その結果は超音速層流制御の妥当性を示した。線形安定性理論にもとづいて、境界層安定解析コードを開発し、その妥当性を2次元の境界層について確認した。風洞試験結果のひとつを解析し、擾乱の特性を明らかにした。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Supersonic wind tunnel tests and numerical analyses were carried out on the boundary layer stability. Wind tunnel tests were performed on a swept wing model. Boundary layer transition locations were detected at various angles of attack and extensions of laminar flow regions by boundary layer suction were also observed. Consequently, the validity of supersonic laminar flow control was suggested. And a boundary layer stability analyses code was developed, based on the linear stability theory, and its validity was confirmed for two dimensional boundary layers. Then one of the wind tunnel test cases was analyzed, and characteristics of disturbances were clarified.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000440006","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-31","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":"富士重工業"},{"subitem_text_value":"富士重工業"},{"subitem_text_value":"富士重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd"},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries, Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"吉田, 茂雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中野, 欣也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塩沢, 信秋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yoshida, Shigeo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakano, Kinya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shiozawa, Nobuaki","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp0031006.pdf","filesize":[{"value":"427.8 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0031006.pdf","url":"https://jaxa.repo.nii.ac.jp/record/36829/files/nalsp0031006.pdf"},"version_id":"4b208011-6521-4f1f-a43d-60149399237b"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"圧縮性層流制御","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層安定性","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"後退翼モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移位置","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層吸気","subitem_subject_scheme":"Other"},{"subitem_subject":"層流域","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速層流制御","subitem_subject_scheme":"Other"},{"subitem_subject":"線形安定性理論","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層安定解析コード","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元境界層","subitem_subject_scheme":"Other"},{"subitem_subject":"擾乱","subitem_subject_scheme":"Other"},{"subitem_subject":"compressible laminar flow control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer stability","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swept wing model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition location","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer suction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow region","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic laminar flow control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear stability theory","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer stability analysis code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional boundary layer","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":"eng"}]},"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":"An experimental and numerical study on the compressible laminar flow control","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An experimental and numerical study on the compressible laminar flow control","subitem_title_language":"en"}]},"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":"36829","relation_version_is_last":true,"title":["An experimental and numerical study on the compressible laminar flow control"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:49:39.786459+00:00"}