{"created":"2023-06-20T15:14:45.388647+00:00","id":44752,"links":{},"metadata":{"_buckets":{"deposit":"424ca67a-a28b-444f-a6ed-1dcc6707a4de"},"_deposit":{"created_by":1,"id":"44752","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44752"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044752","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["471072","471068","471069","471070","471071","471073"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurements of the Unsteady Aerodynamic Derivatives by Forced Oscillation method and Examination of the Dynamic Gust Wind Tunnel Experiments"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1977-04","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"16","bibliographicVolumeNumber":"499","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-499","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突風風胴を用いた,動的全機模型の強制振動法による非定常空気力微係数の実験測定を行ない,その結果と以前の実験結果2)～3)を綜合し,縦の短周期突風応答に対する解析システム群の検討を行なった。また非定常空気力測定実験を最後とした,同じ動的模型による一連の縦の突風応答実験の成果と問題点を総括する。一連の実験の成果は,突風風胴における力学的相似模型(超軽量動的応答模型システム)による半自由飛行突風応答シミュレーションの成功,模型の実験非定常空気力(突風入力と応答運動空気力)を用いた線型微小擾乱近似解析システムの検証,デジタル化統計データ処理,突風応答水平尾翼負荷における特異現象の発見等である。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Measurements of the Unsteady Aerodynamic Derivatives of a dynamic wind tunnel model(1/10 kinematically semi-scaled model of Beech Queen Air) by forced oscillation method are presented. Next, these results are used with other experimental results for the overall system examination of short periods gust response characteristics of the model in the NAL Gust Wind Tunnel. Examination is based on the verification of analytical system of equation of motion using previous experiments. The results confirmes the conventionally used analytical approximations and the success of the dynamic model experiments in the gust wind tunnel. In conclusion, the gains and problems through the series experiments are summarized.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0499000","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-499","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新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"},{"subitem_text_value":"航空宇宙技術研究所新型航空機研究グループ"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"V/STOL Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"V/STOL Aircraft Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"V/STOL Aircraft Research Group, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"西村, 博史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松下, 洸"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"北村, 清美"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NISHIMURA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"MATSUSHITA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KITAMURA, Kiyomi","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":"naltr00499.pdf","filesize":[{"value":"2.9 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00499.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44752/files/naltr00499.pdf"},"version_id":"367ca680-0543-43d0-9c4a-5e1310431f85"}]},"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":"強制振動法による非定常空力係数の測定と突風応答実験の総合的検討","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"強制振動法による非定常空力係数の測定と突風応答実験の総合的検討"}]},"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":"44752","relation_version_is_last":true,"title":["強制振動法による非定常空力係数の測定と突風応答実験の総合的検討"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:51:27.577545+00:00"}