{"created":"2023-06-20T15:15:21.525470+00:00","id":45432,"links":{},"metadata":{"_buckets":{"deposit":"c451d778-6e40-4d48-92ca-0fa65d10d27e"},"_deposit":{"created_by":1,"id":"45432","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"45432"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00045432","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["474798","474789","474796","474791","474790","474792","474794","474793","474795","474797"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental Investigation of High Lift Device for SST"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2002-01","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"33","bibliographicVolumeNumber":"1450","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-1450","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"高揚力装置（内翼前縁フラップ、外翼前縁フラップおよび後縁フラップ）付きSST形態で風洞実験を行い、離着陸性能に関する各種フラップの有効性を検討した。空気力測定と翼表面圧力測定を行い、各種フラップを単独で操舵した場合や複数のフラップを組合せて操舵した場合のフラップの効果について調べた。オイル・フローや煙による流れの可視化を行うことによって翼周りの流れを把握し、空気力や圧力測定結果との対応を試みた。内翼前縁フラップや外翼前縁フラップ単独では揚抗比L/Dの改善はわずかであった。後縁フラップは揚力係数が大幅に増加するとともに、後縁フラップ舵角が小さい場合では大幅なL/Dの改善も得られた。前縁フラップと後縁フラップを組合せて操舵した場合ではさらに大幅なL/D改善が実現でき、前縁フラップと後縁フラップを組合せて操舵した場合は前縁フラップ、後縁フラップ単独操舵による効果を足し合わせた場合よりL/Dの改善幅の大きい結果が得られた。L/Dや揚力係数における各種フラップの有効性をまとめるとともに、これらの実験結果を利用してL/Dにおける最適フラップ舵角に関する知見を得た。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Wind tunnel tests were conducted to investigate the aerodynamic characteristics of an SST model with leading-edge and trailing-edge flaps. Force measurement and surface pressure measurement were performed for the SST model with leading-edge flaps or with trailing-edge flaps and with both flaps deflected. Flow patterns on the upper surface of the model were visualized by means of oil-flow and smoke. Lift-to-drag ratio of the model was improved by leading-edge flap deflection. Deflecting the trailing-edge flap increased lift, drag and pitch-down moment drastically. When the trailing-edge flap was deflected to ten degrees, lift-to-drag ratio could also be improved. The combined effects of leading-edge and trailing-edge flaps were discussed by comparison with the linearly combined measurement results when the leading-edge and trailing-edge flaps were deflected separately.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR1450000","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-1450","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":"1347-4588","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00311347","subitem_source_identifier_type":"NCID"}]},"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次世代超音速機プロジェクトセンター"},{"subitem_text_value":"東京大学大学院"},{"subitem_text_value":"航空宇宙技術研究所次世代超音速機プロジェクトセンター"},{"subitem_text_value":"東京大学工学系研究科"},{"subitem_text_value":"東京大学工学系研究科"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Next Generation SST Project Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Graduate School, The University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Next Generation SST Project Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"郭, 東潤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮田, 勝弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"砂田, 保人"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"李家, 賢一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KWAK, Dong-Youn","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MIYATA, Katsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NOGUCHI, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SUNADA, Yasuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"RINOIE, Kenichi","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":"naltr0001450.pdf","filesize":[{"value":"2.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001450.pdf","url":"https://jaxa.repo.nii.ac.jp/record/45432/files/naltr0001450.pdf"},"version_id":"02820995-2519-4fe0-8766-90ecb0e0bfac"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"SST, Leading-edge Flap, Vortex Flap, Trailing-edge Flap","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"超音速航空機(SST)形態の高揚力装置に関する実験的研究","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速航空機(SST)形態の高揚力装置に関する実験的研究"}]},"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":"45432","relation_version_is_last":true,"title":["超音速航空機(SST)形態の高揚力装置に関する実験的研究"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:39:29.855301+00:00"}