{"created":"2023-06-20T15:02:37.148221+00:00","id":31709,"links":{},"metadata":{"_buckets":{"deposit":"06eeb08f-9022-4e40-b3af-dc08052d6036"},"_deposit":{"created_by":1,"id":"31709","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31709"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031709","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["405833","405831","405830","405829","405832","405828"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"The Effects of Nose Configurations and Free Stream Velocities on Vortex Wake behind Inclined Body of Revolution"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-02","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_A","bibliographicPageEnd":"52","bibliographicPageStart":"35","bibliographicVolumeNumber":"13","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":"飛しょう体背面に発生する渦後流(vortex Wake)が,頭部形状,主流速度によってどのように変動するかが調べられた。実験は4つの頭部形状に対して,迎角O゜から30°の範囲で超音速(M_∞=2)と低速(U_∞=1.1m/sec)の二つの流速に対してなされた。その結果,渦後流の大きさと形状は主流速度や頭部形状にはほとんど無関係であり,迎角と飛しょう体先端からの距離とによって一意的に決定できる事がわかった。又,交差流流速M_∞sinαが,渦後流の構造を決める重要なパラメータである事が明らかになった。しかし,構造上の変化とM_∞sinαとの定量的な関係はつかむ事はできなかった。","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The effect of flow condition and nose configuration on the structure, dimension and shape of vortex wake behind an inclined body of revolution has been investigated by a series of experiments at supersonic and subsonic speeds in the range of angle of attack between 0° to 30° for four nose configurations. The results indicate that the dimension and shape of the vortex wake on the after-body are almost uniquely determined only by the angle of attack and the distance from the apex of the body without being dependent on the nose configuration and the free stream velocity. It is also found that the cross flow velocity M_∞ sin α is one of the important parameters determining the structure of vortex wake, which generally consists of main two vortices, vortex feeding sheets and other small vortices and the effects of vortex feeding sheets and secondary vortices increase with M_∞ sinα.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124730000","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":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Bulletin of the Institute of Space and Aeronautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中尾, 晨一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"並木, 道義"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河村, 龍馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAO, Shin-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAMIKI, Michiyoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMURA, Ryuma","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124730.pdf","filesize":[{"value":"3.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124730.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31709/files/SA0124730.pdf"},"version_id":"3665bc0d-289d-4e5b-99f2-9a94ec62bc07"}]},"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":"飛しょう体背面の渦後流への頭部形状及び主流速度の影響について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"飛しょう体背面の渦後流への頭部形状及び主流速度の影響について"}]},"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":"31709","relation_version_is_last":true,"title":["飛しょう体背面の渦後流への頭部形状及び主流速度の影響について"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:52:46.339035+00:00"}