{"created":"2023-06-20T15:10:09.837652+00:00","id":39764,"links":{},"metadata":{"_buckets":{"deposit":"ed955ca2-ebc9-43e8-b755-db06d8ad905a"},"_deposit":{"created_by":1,"id":"39764","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"39764"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00039764","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["444258","444261","444259","444260"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Evaluation of the flying qualities of the flight research airplane Do228 using V-gamma diagram"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1996-04","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"19","bibliographicPageStart":"1","bibliographicVolumeNumber":"1288","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":"航空宇宙技術研究所の実験用航空機であるドルニエ社製Do228型機の飛行試験データからV-γ線図を作成し、同図を用いて飛行性能値のみでなく縦の運動を支配する主要なパラメータ(縦の微係数)を推定した。また、同機の風洞試験データをもとにした数学モデルより算出したパラメータと飛行試験から得られたV-γ線図により算出されたパラメータとを比較し、数学モデルの検証を行った。さらに、縦の微係数に含まれる誤差の影響を論じた。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this study, the flying qualities of the flight research airplane Do228 were evaluated. By performing some flight tests using a Do228, the V-gamma diagrams with some configurations were drawn out. The flight performance was obtained, and some longitudinal aerodynamic derivatives such as X(sub )u, X(sub w), Z(sub u) and Z(sub w) were estimated from the performance. The parameter errors were examined by comparing the above parameters with those based on the wind tunnel tests. According to the results, the accuracy of the parameters estimated from V-gamma diagrams was sufficient to discuss the longitudinal dynamics.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0000447000","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-1288","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 飛行実験部"},{"subitem_text_value":"航空宇宙技術研究所 飛行実験部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory Flight Research Division"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"穂積, 弘毅"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"坂井, 紀穂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Hozumi, Koki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakai, Toshiho","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":"naltr01288.pdf","filesize":[{"value":"2.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr01288.pdf","url":"https://jaxa.repo.nii.ac.jp/record/39764/files/naltr01288.pdf"},"version_id":"2f35b3ad-2b8c-46eb-89a1-4bef16adbc1c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"実験用航空機","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行性評価","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行包囲線図","subitem_subject_scheme":"Other"},{"subitem_subject":"V-ガンマ線図","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行試験","subitem_subject_scheme":"Other"},{"subitem_subject":"対気速度","subitem_subject_scheme":"Other"},{"subitem_subject":"経路角","subitem_subject_scheme":"Other"},{"subitem_subject":"ピッチ安定化方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"縦空力微係数","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"数学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"Do228","subitem_subject_scheme":"Other"},{"subitem_subject":"flight research airplane","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flying quality evaluation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight envelope","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"V gamma diagram","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"equivalent air speed","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight path angle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pitch stabilized equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"longitudinal aerodynamic derivatives","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"mathematical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Do228","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":"V-γ線図による実験用航空機Do228の飛行性評価","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"V-γ線図による実験用航空機Do228の飛行性評価"}]},"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":"39764","relation_version_is_last":true,"title":["V-γ線図による実験用航空機Do228の飛行性評価"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:19:22.969646+00:00"}