{"created":"2023-06-20T15:15:16.468535+00:00","id":45346,"links":{},"metadata":{"_buckets":{"deposit":"c2807ac6-5bbd-4ab6-b8ac-9e618da7d4fe"},"_deposit":{"created_by":1,"id":"45346","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45346"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045346","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474268","474264","474261","474262","474267","474263","474266","474265"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Velocity Measurements inside the Leading Edge Vortex Formed on a Dalta Wing"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-11","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"18","bibliographicVolumeNumber":"1087","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1087","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"デルタ翼上に生ずる前縁剥離渦の三次元的挙動を把握するために実験を行った。実験に使用した模型は後退角60度の平板デルタ翼である。まず剥離渦の挙動を知るために六分カ測定,表面圧力測定,オイルフロー法とレーザーライトシート法による流れの可視化を行った。次にレーザー2焦点流速度計を用いて剥離渦内部の三次元平均流速分布と速度変動分布を測定した。その結果二次剥離渦の流れ場の様子や,剥離渦内の平均流速分布と速度変動分布との関係が明らかになった。またレーザー2焦点流速計を用いる際の測定誤差や計測方法の問題点についても検討した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Measurements were made to investigate the three dimensional structure of the leading edge vortex formed on a delta wing with a 60deg sweep. The behavior of the vortex was studied by means of a lift measurement, surface pressure measurements and flow visualization tests. Mean velocities and velocity fluctuations were measured using a laser two-focus velocimeter(L2F). In this paper, the flow pattern inside the secondary separation vortex is shown from the results of the above measurements. The relation ship between the mean velocities and the velocity fluctuations are also shown. Since this was the first time L2F had been usde in the NAL gust wind tunnel, the problem of the present experimental method using the L2F is discussed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1087000","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL TR-1087","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Advanced　Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Advanced　Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Advanced　Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Advanced　Aircraft Research Group, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"李家, 賢一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"岩崎, 昭人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤田, 敏美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"藤枝, 郭俊"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"RINOIE, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"IWASAKI, Akihito","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJITA, Toshimi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"FUJIEDA, Hirotoshi","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr01087.pdf","filesize":[{"value":"2.0 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01087.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45346/files/naltr01087.pdf"},"version_id":"b7f865c9-0948-4a48-8890-fef37666021d"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"デルタ翼上に生ずる前縁剥離渦の断面内平均流速等の測定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"デルタ翼上に生ずる前縁剥離渦の断面内平均流速等の測定"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"45346","relation_version_is_last":true,"title":["デルタ翼上に生ずる前縁剥離渦の断面内平均流速等の測定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:41:01.886313+00:00"}