{"created":"2023-06-20T14:37:25.697230+00:00","id":3836,"links":{},"metadata":{"_buckets":{"deposit":"5342d49b-8244-4b27-b8f4-b5eb9884b952"},"_deposit":{"created_by":1,"id":"3836","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3836"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003836","sets":["1398:1530:1535","1543:1874:1879","1887:1891","9:789:855:859"]},"author_link":["16157","16156","16154","16155"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Validation of γ-Reθ Transition Model for the Supersonic Boundary-layer on Cones"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2015-03-25","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"6","bibliographicPageStart":"1","bibliographicVolumeNumber":"JAXA-SP-14-010","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium","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":"第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県","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":"46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The γ-Reθ Transition Model was applied to predict the supersonic boundary-layer transition on cones and the results were compared with flight experiments and wind tunnel ones. The model failed to predict important effects in high Mach number flows, i.e. higher mode instability, heat transfer and entropy layer. Although the prediction accuracy of the current γ-ReθTransition Model in high Mach number flows is not good, the distinctive advantages of the model such as low computation load and suitability for parallel computing are desirable and should be maintained in improvement to come. Fundamental data to make the correlation which involves the effects of Mach number, heat-transfer, entropy layer and cross-flow etc. are needed.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA1530023001","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: JAXA-SP-14-010","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","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":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"株式会社IHIエスキューブ"},{"subitem_text_value":"株式会社IHIエアロスペース"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"IHI Scube Co., Ltd."},{"subitem_text_language":"en","subitem_text_value":"IHI AEROSPACE CO., LTD."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"棟石, 篤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宇賀神, 裕樹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Muneishi, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ugajin, Hiroki","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":"2020-01-16"}],"displaytype":"detail","filename":"AA1530023001.pdf","filesize":[{"value":"683.3 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1530023001.pdf","url":"https://jaxa.repo.nii.ac.jp/record/3836/files/AA1530023001.pdf"},"version_id":"671c413b-9725-499a-9c02-f8c7c80ddce2"}]},"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":"超音速流れ中の円錐上境界層におけるγ-Reθ遷移モデルの検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速流れ中の円錐上境界層におけるγ-Reθ遷移モデルの検証"}]},"item_type_id":"5","owner":"1","path":["859","1535","1879","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-04-28"},"publish_date":"2015-04-28","publish_status":"0","recid":"3836","relation_version_is_last":true,"title":["超音速流れ中の円錐上境界層におけるγ-Reθ遷移モデルの検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:53:54.360062+00:00"}