{"created":"2023-06-20T15:16:14.450916+00:00","id":46351,"links":{},"metadata":{"_buckets":{"deposit":"b4de9416-ffb8-497a-a547-d67c917c5161"},"_deposit":{"created_by":1,"id":"46351","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"46351"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00046351","sets":["1398:1530:2040","1543:1874:2045","1887:1891","9:789:790:2039"]},"author_link":["514083","514082"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Effect of the disturbance velocity component on jet diffusion in a supersonic jet"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2020-02-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"139","bibliographicPageStart":"135","bibliographicVolumeNumber":"JAXA-SP-19-007","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第51回流体力学講演会/第37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 51st Fluid Dynamics Conference / the 37th 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51回流体力学講演会/第37回航空宇宙数値シミュレーション技術シンポジウム (2019年7月1日-3日. 早稲田大学早稲田キャンパス国際会議場), 新宿区, 東京","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":"51st Fluid Dynamics Conference / the 37th Aerospace Numerical Simulation Symposium (July 1-3, 2019. International Conference Center, Waseda University), Shinjuku-ku, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The three-dimensional compressible Navier-Stokes equations are numerically solved to study effect of the velocity component of inflow disturbance on receptivity of helical mode in a supersonic round jet at high convective Mach numbers. Initial disturbances with only u(sub r), u(sub θ) and u(sub x) velocity components are compared. The numerical results show that the inflow disturbance of the only u(sub r) component is easily accepted into the jet as the helical mode than the case of the only u(sub θ) component and u(sub x) component without azimuthal wave number dependency. In addition, the magnitudes of the pressure fluctuations emitted from the jet are approximately equal when the diffusion start time of the jet is the same. There are less dependence of initial condition's velocity component in the jet sound field.","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: AA1930011010","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-19-007","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_22":{"attribute_name":"ISSNONLINE","attribute_value_mlt":[{"subitem_source_identifier":"2433-2232","subitem_source_identifier_type":"ISSN"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"富山大学"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"University of Toyama"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"渡辺, 大輔"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watanabe, Daisuke","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":"2020-03-27"}],"displaytype":"detail","filename":"AA1930011010.pdf","filesize":[{"value":"820.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"AA1930011010.pdf","url":"https://jaxa.repo.nii.ac.jp/record/46351/files/AA1930011010.pdf"},"version_id":"0bc7c7c3-653c-4b42-9419-9086d62ad9ad"}]},"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":"超音速ジェットの拡散に及ぼす撹乱速度成分の影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速ジェットの拡散に及ぼす撹乱速度成分の影響"}]},"item_type_id":"5","owner":"1","path":["1891","2039","2040","2045"],"pubdate":{"attribute_name":"公開日","attribute_value":"2020-02-04"},"publish_date":"2020-02-04","publish_status":"0","recid":"46351","relation_version_is_last":true,"title":["超音速ジェットの拡散に及ぼす撹乱速度成分の影響"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T20:13:33.030656+00:00"}