{"created":"2023-06-20T15:11:31.027639+00:00","id":41193,"links":{},"metadata":{"_buckets":{"deposit":"50b6add3-2968-4003-8622-7b5e9f2057a5"},"_deposit":{"created_by":1,"id":"41193","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41193"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041193","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["451080","451085","451073","451076","451077","451081","451079","451083","451086","451072","451078","451087","451075","451084","451074","451082"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"On the aeroelastic characteristics of the forward swept wing optimized by aeroelastic tailoring"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1993-07","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"1","bibliographicVolumeNumber":"1208","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":"空力弾性テイラリングで最適化された前進翼の遷音速領域でのフラッタ限界値を、迎角0度の場合と2度の場合の一部について実験的に確認したので報告する。迎角2度の場合(設計点)ではテイラリングされた最適化前進翼は、極めて接近した動圧で2つのモードのフラッタとダイバージェンスがほぼ同時に起きることが確認された。最適化された翼としての観点から非常に興味深い現象である。さらに以前から行われているパラメタスタディとの結果とも比較がなされている。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Research on Aeroelastic Tailoring at NAL is presented. Flutter boundaries for an optimized forward swept wing have been experimentally verified at angles of attack of zero deg and two deg (which is the design point) in the transonic range. It was found that two different mode flutters and a divergence occur at almost the same dynamic pressure for the optimized forward swept wing. The aeroelastic behaviors of the optimized forward swept wing are investigated and are compared with those of parametric studies performed previously.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004223000","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-1208","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 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 構造力学部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"},{"subitem_text_value":"航空宇宙技術研究所 機体部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Structural Mechanics Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Airframe Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"江尻, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"菊池, 孝男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"峯岸, 正勝"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"外崎, 得雄"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"熊倉, 郁夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野口, 義男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"磯貝, 紘二"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ejiri, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kikuchi, Takao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Minegishi, Masakatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sotozaki, Tokuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kumakura, Ikuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Noguchi, Yoshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Isogai, Koji","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":"naltr01208.pdf","filesize":[{"value":"1.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01208.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41193/files/naltr01208.pdf"},"version_id":"952eaf4a-5ef1-42ee-a84f-eb25905a0397"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力弾性テーラリング","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性最適化","subitem_subject_scheme":"Other"},{"subitem_subject":"空力弾性スケールモデル","subitem_subject_scheme":"Other"},{"subitem_subject":"前進翼","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ限界","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ試験","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタモード","subitem_subject_scheme":"Other"},{"subitem_subject":"翼ダイバージェンス","subitem_subject_scheme":"Other"},{"subitem_subject":"遷音速空気力学","subitem_subject_scheme":"Other"},{"subitem_subject":"主翼空力設計","subitem_subject_scheme":"Other"},{"subitem_subject":"複合材箱型桁","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波失速フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelastic tayloring","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelastic optimization","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelastic scale model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"swept forward wing","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter boundary","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter mode","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing divergence","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"transonic aerodynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wing aerodynamic design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"composite material box spar","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock stall flutter","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":"空力弾性テイラリングによって最適化された前進翼の空力弾性特性について","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"空力弾性テイラリングによって最適化された前進翼の空力弾性特性について"}]},"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":"41193","relation_version_is_last":true,"title":["空力弾性テイラリングによって最適化された前進翼の空力弾性特性について"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:12:20.478754+00:00"}