{"created":"2023-06-20T15:02:59.968401+00:00","id":32089,"links":{},"metadata":{"_buckets":{"deposit":"6bb1b8f4-ce5f-4605-8841-56ac56df33e1"},"_deposit":{"created_by":1,"id":"32089","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32089"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032089","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["407246","407247","407250","407249","407245","407248"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"An Experimental Investigation on Secondary Side-Jet Injection in Supersonic Free Stream"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1969-07","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"3","bibliographicPageEnd":"475","bibliographicPageStart":"463","bibliographicVolumeNumber":"5","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"鋭い前縁をもつ平板に設けたスリットから,二次空気流を主流に垂直方向に噴射させたときの,主流との干渉現象についての報告である.スリットは平板の中央付近にあり,噴射口で音速状態が達成される.主流マッハ数は2および3.主流および噴射流条件,ならびにスリットから前縁までの距離を種々変化させて実験を行なった.スリットから前縁までの距離を変化させると,平板上の流れ方向の圧力分布の形状のうち,スリットの上流側のみに差異が現われることがわかった.また,力,モーメント,風圧中心の様な積分量は,二次流と主流の運動量比で整理でき,スリットの上流側のみならず,下流側の圧力分布にも強く依存することがわかった.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Present paper gives the experimental results of the aerodynamic interaction phenomena between a secondary air jet and a primary supersonic flow of Mach numbers 2 and 3. The models used are flat plates with a sharp leading edge having a slit at some distance from the leading edge. The secondary jet is injected perpendicularly to the main flow at sonic jet velocity. The parameters varied are the main and the secondary flow conditions as well as the distance from the leading edge to the slit. It is observed that appreciable change in pressure distribution appears only in the upstream part of the slit due to the change of the distance from the leading edge to the slit. It becomes clear that integrated quantities such as force, moment and centre of pressure on the flat plate in various cases of experiment are well arranged by using the ratio of the secondary to the main flow momentum, and that their depending on the downstream part of the slit is not small compared to that on the upstream.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125192000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学大学院"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeronautical Science"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河村, 龍馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関, 和市"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 信夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMURA, Ryuma","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SEKI, Kazuichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IWASAKI, Nobuo","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":"SA0125192.pdf","filesize":[{"value":"742.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125192.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32089/files/SA0125192.pdf"},"version_id":"a1fa5505-072c-4330-a219-09226deb8b56"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"超音速における側方二次噴射に関する実験的研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速における側方二次噴射に関する実験的研究"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32089","relation_version_is_last":true,"title":["超音速における側方二次噴射に関する実験的研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:41:21.896425+00:00"}