{"created":"2023-06-20T15:03:08.464020+00:00","id":32264,"links":{},"metadata":{"_buckets":{"deposit":"2cbb24c8-31e5-41d7-8f18-4e2caa09f03e"},"_deposit":{"created_by":1,"id":"32264","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"32264"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00032264","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["408014","408015","408016","408017"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Measurement of the Drag of the Body Immersed in a High Speed Rarefied Gas Flow by the Suspension Method"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1971-04","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2_A","bibliographicPageEnd":"423","bibliographicPageStart":"414","bibliographicVolumeNumber":"7","bibliographic_titles":[{"bibliographic_title":"東京大学宇宙航空研究所報告"}]}]},"item_9_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"低密度風洞で,吊下げ法による球の抵抗測定から,抵抗係数を既知として,気流の動圧決定を試みた.実験条件は気流マッハ数2,0～3.5,長さ1cmに対するレイノルズ数50～250である.同じ吊下げ法で,頭部が円形および正方形状の非常に軽い発泡スチロール製模型の抵抗係数を求め,レイノルズ数による変化ならびに形状による相異を示した.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An attempt has been made of the determination of dynamic pressure in the low density wind tunnel by measuring the drag force exerted on a sphere with the wire suspension system and using the drag coefficient of sphere given by the empirical formula. The flow conditions of the present tests are in the Mach number range of 2.0～3.5 and in the Reynolds number range of 50～250 for the length of 1cm. With the same system, the drag forces experienced by ultralightweight models of foamed plastics with circular and square-flat noses have been measured. The effects of the Reynolds number and the shape of model on the drag coefficient have been examined.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0125428000","subitem_description_type":"Other"}]},"item_9_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"東京大学宇宙航空研究所"}]},"item_9_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0563-8100","subitem_source_identifier_type":"ISSN"}]},"item_9_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00161914","subitem_source_identifier_type":"NCID"}]},"item_9_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"東京大学宇宙航空研究所"},{"subitem_text_value":"東京大学宇宙航空研究所"}]},"item_9_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"},{"subitem_text_language":"en","subitem_text_value":"Institute of Space and Aeroautical Science University of Tokyo"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"雛田, 元紀"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"寺田, 守男"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HINADA, Motoki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TERADA, Morio","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":"2020-01-24"}],"displaytype":"detail","filename":"SA0125428.pdf","filesize":[{"value":"929.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0125428.pdf","url":"https://jaxa.repo.nii.ac.jp/record/32264/files/SA0125428.pdf"},"version_id":"4287e1c7-d82d-43b7-92f5-066fb7ee03e9"}]},"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":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"吊下げ法による高速希薄気流中の物体の抵抗測定","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"吊下げ法による高速希薄気流中の物体の抵抗測定"}]},"item_type_id":"9","owner":"1","path":["1890","1910"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"32264","relation_version_is_last":true,"title":["吊下げ法による高速希薄気流中の物体の抵抗測定"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:36:58.277240+00:00"}