{"created":"2023-06-20T15:13:49.902280+00:00","id":43804,"links":{},"metadata":{"_buckets":{"deposit":"04543a61-60a5-4882-bb0c-70b0d21e1751"},"_deposit":{"created_by":1,"id":"43804","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43804"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043804","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465677","465670","465672","465674","465671","465676","465673","465675"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurement of the Dynamic Stability Derivatives of Rocket Configuration Models"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1972-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"21","bibliographicVolumeNumber":"221","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":"Longitudinal dynamic stability derivatives of NAL-7 rocket models of different body  length are measured by a longitudinal dynamic test and a roll dynamic test with angles of   attack in wind tunnels at M=0.  6・2. 0 and by free  flight test. Both the results of wind  tunnels and of free flight test are compard, and they show fairly good agreement.  Another rocket configuration models are also tested in wind tunnels at M=0.6,--3.0.     Roll damping derivatives of these models are measured at the same Mach number range.  Some of these results show the interaction of wing to wing at subsonic and low super- sonic ranges. At the range of M 1.2, the experimental data agree precisely with the  calculated values.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0221000","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-221","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2部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第2部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第2部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第2部"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高島, 一明"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"谷, 喬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 正剛"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAKASHIMA, Kazuaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TANI, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SEKINE, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAMURA, Seigo","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":"naltm00221.pdf","filesize":[{"value":"3.6 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00221.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43804/files/naltm00221.pdf"},"version_id":"b61b0818-a93f-47a7-b2a1-200f29315192"}]},"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":"ロケット模型の動安定微係数の測定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ロケット模型の動安定微係数の測定"}]},"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":"43804","relation_version_is_last":true,"title":["ロケット模型の動安定微係数の測定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:07:35.686256+00:00"}