{"created":"2023-06-20T15:13:47.771562+00:00","id":43762,"links":{},"metadata":{"_buckets":{"deposit":"3c5622f4-b7f0-4db5-ab26-ee50b0a0de8e"},"_deposit":{"created_by":1,"id":"43762","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43762"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043762","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["465462","465461","465458","465455","465456","465457","465459","465460"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Apparatus for Measuring Dynamic Stability Derivatives in NAL 6m Law-speed Wind-tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1970-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"17","bibliographicVolumeNumber":"178","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":"A forsed-oscillation apparatus for measuring dynamic stability derivatives has been completed in NAL 6m low-speed wind-tunnel.This appartus is capable of forcing a model to perform a single-degree-of-freedom angular oscillation about its pitch, yow, and roll axes with maximum frecuency of 1 Hz and with maximum amplitude of 10°, by means of a 30-PS variable-frequency electric moter and a crank mechanism.The output of the balance inserted in the model, is processed by an analogue readout system utilizing a manually-adjusted null method.The results of the tests which were carried out to confirm the reliability of this method using a conventional airplane model, revealed that it was satisfactory.Some of the difficulties affecting the accuracy of the test are discussed.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0178000","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-178","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 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Kan-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ENDO, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OKABE, Yujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TODA, Nobuhiro","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":"naltm00178.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00178.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43762/files/naltm00178.pdf"},"version_id":"044c1f92-e835-4861-af3a-46520931818e"}]},"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":"大型低速風胴動安定微係数測定装置","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大型低速風胴動安定微係数測定装置"}]},"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":"43762","relation_version_is_last":true,"title":["大型低速風胴動安定微係数測定装置"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:08:21.826734+00:00"}