{"created":"2023-06-20T15:14:29.172234+00:00","id":44480,"links":{},"metadata":{"_buckets":{"deposit":"b2fecfc2-1554-46b6-ade3-40fea6637684"},"_deposit":{"created_by":1,"id":"44480","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44480"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044480","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["469676","469669","469670","469671","469672","469673","469674","469677","469675","469668"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Free Flight Tests on Longitudinal Dynamic Characteristics of FFM-10 Model"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1971-07","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"20","bibliographicVolumeNumber":"237","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-237","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Free Flight Model FFM-10 is a model which simulates a supersonic aircraft with delta wing. The model is propelled by a rocket motor installed in the fuselage. Longitudinal short period motion is excited by two side-jets ignited in sequence. Measurements of acceleration in the direction of pitching motion enable the determination of longitudinal static and dynamic aerodynamic derivatives. The results are compared with theoretical estimates and show fairly food agreement. Although much improvement should be pursued to obtain satisfactory accuracy, the preliminary results show that the technique employed is very promising.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0237000","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-237","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宇宙研究グループ"},{"subitem_text_value":"航空宇宙技術研究所機体第二部"},{"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_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Space Technology Research Group, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Airframe Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Flight Research Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河崎, 俊夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"塙, 武敏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"斎藤, 秀夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高島, 一明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河本, 巌"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWASAKI, Toshio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HANAWA, Taketoshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SAITO, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKASHIMA, Kazuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMOTO, Iwao","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":"naltr00237.pdf","filesize":[{"value":"4.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00237.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44480/files/naltr00237.pdf"},"version_id":"dee204ef-d9da-44cd-bf8e-5638893349bd"}]},"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":"自由飛行模型FFM-10による縦の動安定特性の飛しょう実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"自由飛行模型FFM-10による縦の動安定特性の飛しょう実験"}]},"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":"44480","relation_version_is_last":true,"title":["自由飛行模型FFM-10による縦の動安定特性の飛しょう実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:56:16.727242+00:00"}