{"created":"2023-06-20T15:11:01.667892+00:00","id":40612,"links":{},"metadata":{"_buckets":{"deposit":"f228bcff-b76e-4ed6-926d-3e93ce5c6e10"},"_deposit":{"created_by":1,"id":"40612","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"40612"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00040612","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["448870","448869","448871","448872","448873","448868"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"遷音速流内の3次元HLFC翼の空力特性"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-05","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"23","bibliographicPageStart":"1","bibliographicVolumeNumber":"1385T","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":"自然層流翼型に組み込んだ前縁吸い込みシステムを持つハイブリッド(HLFC)層流制御翼模型の、主に遷音速マッハ数における抵抗低減効果を確認するために、風洞試験を行った。その結果、本システムは設計、非設計条件の如何にかかわらず、きわめてわずかな吸い込みにより、大きなウエーク抵抗の減少を与えることが確認された。この抵抗低減効果のほかに本試験では、かなり広いマッハ数領域において、ある範囲の吸い込み量に対して揚力が吸い込み無しの時より増加することが見いだされた。この揚力の増加は、抵抗の低減だけから期待されるよりはるかに大きな揚抗比の増加をもたらす。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"A transonic wind tunnel test of an HLFC (Hybrid Laminar Flow Control) wing model with a new leading edge suction system incorporated with a natural laminar flow airfoil was conducted to check mainly the drag reducing effect of the suction system in the transonic Mach number range. The test confirmed that the system works well in both design and off-design conditions, resulting in significant drag reduction in a wake drag with even a small amount of suction. Besides the drag reducing effect, it was found that the system produces considerable lift increase for some suction quantity ranges in a wide range of test Mach number. The lift increment generates a higher L/D (overall wing Lift/overall wing Drag) value than that which may be expected from the drag reduction alone.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001976000","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-1385T","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 流体科学総合研究グループ"},{"subitem_text_value":"航空宇宙技術研究所 次世代航空機プロジェクト推進センター"},{"subitem_text_value":"航空宇宙技術研究所 空気力学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Fluid Science Research Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Advanced Technology Aircraft Project Center"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Aerodynamic Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石田, 洋治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 正芳"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"鈴木, 浩一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishida, Yoji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Masayoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Suzuki, Koichi","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":"naltr0001385t.pdf","filesize":[{"value":"2.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr0001385t.pdf","url":"https://jaxa.repo.nii.ac.jp/record/40612/files/naltr0001385t.pdf"},"version_id":"0a6f9723-f2cf-4cae-99e2-2a9902652b7f"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"層流翼","subitem_subject_scheme":"Other"},{"subitem_subject":"3次元翼","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"層流制御","subitem_subject_scheme":"Other"},{"subitem_subject":"抗力低減","subitem_subject_scheme":"Other"},{"subitem_subject":"揚力増加","subitem_subject_scheme":"Other"},{"subitem_subject":"吸込効果","subitem_subject_scheme":"Other"},{"subitem_subject":"空力特性","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"three dimensional wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"laminar flow control","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic lift increase","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"suction effect","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic characteristic","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"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":"Aerodynamic characteristics of a three-dimensional HLFC wing in transonic flow","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Aerodynamic characteristics of a three-dimensional HLFC wing in transonic flow","subitem_title_language":"en"}]},"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":"40612","relation_version_is_last":true,"title":["Aerodynamic characteristics of a three-dimensional HLFC wing in transonic flow"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:14:42.467716+00:00"}