{"created":"2023-06-20T15:14:55.239595+00:00","id":44934,"links":{},"metadata":{"_buckets":{"deposit":"7048c0e4-7744-4ff6-9497-7136c4ffb240"},"_deposit":{"created_by":1,"id":"44934","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44934"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044934","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472037","472038"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"STOL実験機模型の尾翼付近の流れ場"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"28","bibliographicVolumeNumber":"677","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-677","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to improve the weather cock stability derivative Cnβ of the NAL STOL research aircraft model, some surveys of the flow field around the empennage for the STOL landing configuration were carried out. The down wash angle, the side wash angle, and the dynamic pressure at the aerodynamic center of the empennage (25％ mean aerodynamic chord) were obtained by means of linear interpolation of the values measured at the two sections perpendicular to the free stream. Effects of the engine thrust coefficient and the two types of vortex generator on the flow field, and the directional stability in the case of an inner engine becoming inoperative, were studied with reference to the results of the force tests.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0677000","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-677","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"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"STOLプロジェクト推進本部実験機開発室空力技術開発チーム"}],"nameIdentifiers":[{"nameIdentifier":"472037","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Aerodynamics Team  Research Aircraft Development Section  STOL Aircraft Project Group","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"472038","nameIdentifierScheme":"WEKO"}]}]},"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":"naltr00677.pdf","filesize":[{"value":"3.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00677.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44934/files/naltr00677.pdf"},"version_id":"ef5eb365-969f-4eff-81c9-3454a5c27805"}]},"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":"Surveys of Flow-Field around Empennage of the NAL STOL-Research-Aircraft Model","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Surveys of Flow-Field around Empennage of the NAL STOL-Research-Aircraft Model","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":"44934","relation_version_is_last":true,"title":["Surveys of Flow-Field around Empennage of the NAL STOL-Research-Aircraft Model"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:42:47.755375+00:00"}