{"created":"2023-06-20T15:11:30.825379+00:00","id":41189,"links":{},"metadata":{"_buckets":{"deposit":"fb0fdb0c-8b7b-4154-bb51-fa8b5a3bd653"},"_deposit":{"created_by":1,"id":"41189","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41189"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041189","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451054","451059","451058","451057","451055","451052","451056","451053"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"High subsonic and high Reynolds number wind tunnel tests of two-dimensional natural-laminar-flow airfoils with suction boundary layer control"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"14","bibliographicPageStart":"1","bibliographicVolumeNumber":"1204","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"吸い込みのある場合とない場合との抵抗特性を比較するため、多溝性、多孔性および固体面の3種類の表面をもつ自然層流翼型模型につき高亜音速、高レイノルズ数での風洞試験を行った。マッハ数は0.60から0.85まで、レイノルズ数は6×10｛6｝から20×10｛6｝までの範囲とした。試験結果は、気流の乱れ、吸込み用溝や孔の存在などの層流化を妨げる要因があるにも拘わらず、吸い込みにより約10％の抵抗減少が得られることを示した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Wind tunnel tests in high subsonic and high Reynolds number flows were conducted using slotted, perforated, and solid-surface NLF (Natural Laminar Flow) airfoils to compare their drag characteristics with and without suction. The Mach number was varied from 0.6 to 0.85 and the Reynolds number from 6 to 20 million. The results show that a net drag reduction of about 10 percent was attained by suction despite the presence of severe adverse effects against laminarization in the wind tunnel test such as free-stream turbulence and roughness effects of suction holes or slots.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004219000","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-1204","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 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"},{"subitem_text_value":"航空宇宙技術研究所 空力性能部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aircraft Aerodynamics Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"佐藤, 衛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"神田, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 洋治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sato, Mamoru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kanda, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Yoji","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":"2020-01-27"}],"displaytype":"detail","filename":"naltr01204.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01204.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41189/files/naltr01204.pdf"},"version_id":"d00edce6-12c3-4c87-8e4f-357372709def"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"層流制御実験","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層吸い込み","subitem_subject_scheme":"Other"},{"subitem_subject":"自然層流翼型","subitem_subject_scheme":"Other"},{"subitem_subject":"2次元風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"高レイノルズ数風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"ハイブリッド層流制御翼","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層遷移","subitem_subject_scheme":"Other"},{"subitem_subject":"風試模型表面粗さ","subitem_subject_scheme":"Other"},{"subitem_subject":"多孔壁吸い込み","subitem_subject_scheme":"Other"},{"subitem_subject":"多溝壁吸い込み","subitem_subject_scheme":"Other"},{"subitem_subject":"静圧分布計測","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow control experiment","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer suction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"natural laminar flow airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high Reynolds number wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hybrid laminar flow airfoil","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel model surface roughness","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"perforated wall suction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"slotted wall suction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static pressure measurement","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":"吸い込みのある2次元自然層流翼の高亜音速、高Re数風洞試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"吸い込みのある2次元自然層流翼の高亜音速、高Re数風洞試験"}]},"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":"41189","relation_version_is_last":true,"title":["吸い込みのある2次元自然層流翼の高亜音速、高Re数風洞試験"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:24.542910+00:00"}