{"created":"2023-06-20T15:13:47.415882+00:00","id":43757,"links":{},"metadata":{"_buckets":{"deposit":"99dfc3f8-c72e-4ed0-9d64-bd0163bbb3ca"},"_deposit":{"created_by":1,"id":"43757","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43757"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043757","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465432","465430","465433","465426","465429","465431","465428","465427"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Dynamic Stability Derivatives of A Modified FA-200 Airplane"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1970-03","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"12","bibliographicVolumeNumber":"173","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所資料"},{"bibliographic_title":"Technical Memorandum of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The low-subsonic rotary dynamic derivatives of a conventional type of airplane, FA-200 modified, were measured by means of the forced-oscillation apparatus in the NAL 6m low- speed wind-tunnel. The results were compared with the theoretical values calculated by the standard estimation formulae worked out by various authors.  It is shown that the calculated values are in fairly good agreement with the measured ones, except when the separation of air-flow is supplsed to occur on the wings in course of the pitching oscillation. The accuracy of measurement of Cnr was rather low, presumably becacuse the vertical tail moved, crossing the unsteady wake behind the fuselage, in yawing oscillation.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0173000","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 TM-173","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":"0452-2982","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":"AN00314334","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空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"遠藤, 浩"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"林, 良生"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"海老沼, 幸成"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中谷, 輝臣"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ENDO, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HAYASHI, Yoshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"EBINUMA, Yukinari","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAYA, Teruomi","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":"2020-01-28"}],"displaytype":"detail","filename":"naltm00173.pdf","filesize":[{"value":"921.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00173.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43757/files/naltm00173.pdf"},"version_id":"f9c6f5e0-e4c8-4b34-98f7-e4e6193fdac8"}]},"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":"FA-200改機の動安定微係数","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"FA-200改機の動安定微係数"}]},"item_type_id":"3","owner":"1","path":["1893","1916"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43757","relation_version_is_last":true,"title":["FA-200改機の動安定微係数"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:08:27.373679+00:00"}