{"created":"2023-07-25T08:02:58.612916+00:00","id":828,"links":{},"metadata":{"_buckets":{"deposit":"949fa5be-0e63-4a7d-8752-254d65eaa1ed"},"_deposit":{"created_by":18,"id":"828","owners":[18],"pid":{"revision_id":0,"type":"depid","value":"828"},"status":"published"},"_oai":{"id":"oai:ir.kagoshima-u.ac.jp:00000828","sets":["54:92"]},"author_link":["112901","112902","112903","5359","112904"],"item_6_biblio_info_5":{"attribute_name":"収録雑誌名","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1997","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"607","bibliographicPageEnd":"886","bibliographicPageStart":"879","bibliographicVolumeNumber":"63","bibliographic_titles":[{"bibliographic_title":"日本機械学會論文集. B編","bibliographic_titleLang":"ja"}]}]},"item_6_date_6":{"attribute_name":"作成日","attribute_value_mlt":[{"subitem_date_issued_datetime":"1997-03-01","subitem_date_issued_type":"Issued"}]},"item_6_description_4":{"attribute_name":"要約(Abstract)","attribute_value_mlt":[{"subitem_description":"Experiments on the shock wave/turbulent boundary layer interaction were conducted at the free  stream Mach number M1e of 1.97 to 2.50 and the Reynolds number based on the boundary layer  thickness Reδ1 of 3.1 x 10^4 to 5.8 x 10^4 using a supersonic nozzle having a divergent half angle of 10 degrees. Nozzle wall static pressure measurements and the schlieren optical observation of the  interaction region were carried out. Also, the effects of M1e and Reδ1 on the shock-induced turbulent  boundary layer separation were investigated theoretically. As a result, the analytical results of the ratio Ps/P1 of the eparation pressure Ps to the pressure at the onset of the interaction P1 were found to increase with increasing M1e for a fixed Reδ1 and to increase with increasing Reδ1 for a fixed M1e and to provide excellent agreement with the experimental results on the shock-induced turbulent \n boundary layer separation.","subitem_description_language":"en","subitem_description_type":"Other"}]},"item_6_publisher_23":{"attribute_name":"公開者・出版者","attribute_value_mlt":[{"subitem_publisher":"日本機械学会","subitem_publisher_language":"ja"}]},"item_6_relation_11":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_type_id":{"subitem_relation_type_id_text":"https://doi.org/10.1299/kikaib.63.879","subitem_relation_type_select":"DOI"}}]},"item_6_rights_12":{"attribute_name":"権利","attribute_value_mlt":[{"subitem_rights":"日本機械学会","subitem_rights_language":"ja"}]},"item_6_source_id_7":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"03875016","subitem_source_identifier_type":"PISSN"}]},"item_6_source_id_9":{"attribute_name":"NII書誌ID","attribute_value_mlt":[{"subitem_source_identifier":"AN00187441","subitem_source_identifier_type":"NCID"}]},"item_6_subject_15":{"attribute_name":"NDC","attribute_value_mlt":[{"subitem_subject":"423","subitem_subject_scheme":"NDC"}]},"item_6_version_type_14":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"宮里, 義昭","creatorNameLang":"ja"},{"creatorName":"ミヤザト, ヨシアキ","creatorNameLang":"ja-Kana"},{"creatorName":"Miyazato, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"樫谷, 賢士","creatorNameLang":"ja"},{"creatorName":"カシタニ, マサシ","creatorNameLang":"ja-Kana"},{"creatorName":"Kashitani, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"金, 羲東","creatorNameLang":"ja"},{"creatorName":"Kim, Heuy-Dong","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"片野田, 洋","creatorNameLang":"ja"},{"creatorName":"カタノダ, ヒロシ","creatorNameLang":"ja-Kana"},{"creatorName":"Katanoda, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{},{}]},{"creatorNames":[{"creatorName":"松尾, 一泰","creatorNameLang":"ja"}],"familyNames":[{}],"givenNames":[{}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2016-10-27"}],"displaytype":"detail","filename":"AN00187441_v63n607_p879-886.pdf","filesize":[{"value":"27.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AN00187441_v63n607_p879-886.pdf","objectType":"fulltext","url":"https://ir.kagoshima-u.ac.jp/record/828/files/AN00187441_v63n607_p879-886.pdf"},"version_id":"e0faae0c-74f2-4994-8bb8-908d8b5e1a36"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Compressible Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock Wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Separation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic Nozzle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Turbulent Boundary Layer","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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"超音速ノズル内の衝撃波による乱流境界層のはく離","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速ノズル内の衝撃波による乱流境界層のはく離","subitem_title_language":"ja"},{"subitem_title":"チョウ オンソク ノズル ナイ ノ ショウゲキハ ニヨル ランリュウ キョウカイ ソウ ノ ハクリ","subitem_title_language":"ja-Kana"},{"subitem_title":"Shock-Induced Turbulent Boundary Layer Separation in Supersonic Nozzles","subitem_title_language":"en"}]},"item_type_id":"6","owner":"18","path":["92"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2015-04-27"},"publish_date":"2015-04-27","publish_status":"0","recid":"828","relation_version_is_last":true,"title":["超音速ノズル内の衝撃波による乱流境界層のはく離"],"weko_creator_id":"18","weko_shared_id":-1},"updated":"2024-02-07T07:00:09.726578+00:00"}