{"created":"2023-06-20T15:13:48.090598+00:00","id":43767,"links":{},"metadata":{"_buckets":{"deposit":"3f35b6e8-1692-47b7-8118-0b515aeb183b"},"_deposit":{"created_by":1,"id":"43767","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43767"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043767","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465475","465478","465477","465474","465473","465476"],"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1970-09","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"23","bibliographicVolumeNumber":"183","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_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"当所の大型低速風胴において,ロケット模型試験用に製作した小容量の3分力天秤とローリング・モーメント天秤を用いてLS-Cロケット模型および動翼制御用模型について風胴試験を行なったので,その結果について報告する。試験は,LS-Cロケット模型については,風速20,45,60m/secに対し3分力試験を行ない,動翼制御用ロケット模型については,風速45m/secで3分力およびローリング・モーメント試験を行なった。得られた結果を遷超音速風胴試験結果と比較し,十分良好な結果の得られることを確認した。","subitem_description_type":"Abstract"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0183000","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-183","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"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"近藤, 洋史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"高橋, 宏"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"桑野, 尚明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KONDO, Hirofumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKAHASHI, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KUWANO, Naoaki","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":"naltm00183.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00183.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43767/files/naltm00183.pdf"},"version_id":"0881d2cc-026e-406c-a1a5-8ade2b2d3e35"}]},"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":"ロケット模型の大型低速風胴試験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケット模型の大型低速風胴試験"}]},"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":"43767","relation_version_is_last":true,"title":["ロケット模型の大型低速風胴試験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:08:16.001489+00:00"}