{"created":"2023-06-20T15:14:32.053841+00:00","id":44523,"links":{},"metadata":{"_buckets":{"deposit":"4b0d8bed-affa-454f-b34e-3bdf1b543f28"},"_deposit":{"created_by":1,"id":"44523","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44523"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044523","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["469889","469888","469887","469886"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Experimental Study on the Hypersonic Aerodynamic Characteristics of Spherically-Blunted Cones by the Gun Tunnel"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1972-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"15","bibliographicVolumeNumber":"280","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-280","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The drag of a series of spherically-blunted cones made up with three classes of half-vertex angle and five kinds of nose bluntness are measured using the force balance in a hyper-sonic flow obtained by use of the gun tunnel. The flow Mach number and Reynolds number, based on the model length, are 13.6 and 1.2×10(exp 5)-2.4×10(exp 5), respectively. The measured drag is corrected for source flow effect using the measured free-stream Mach number distribution around the model, because it is measured in a flow obtained by a conical hypersonic nozzle and comprises the effect. The viscous effect is also evaluated by the method treated in this paper, in order to compare with results of theoretical inviscid drag. The pressure distribution over a blunted cone in inviscid hypersonic flow, which is obtained from the experimental results of drag of the blunted cones, is compared with results of the inviscid hypersonic theory and other experiments.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0280000","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-280","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空気力学第一部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第一部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"First Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"First Aerodynamics Division, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"曾我, 国男"}],"nameIdentifiers":[{"nameIdentifier":"469886","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小野寺, 信幸"}],"nameIdentifiers":[{"nameIdentifier":"469887","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"SOGA, Kunio","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"469888","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"ONODERA, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"469889","nameIdentifierScheme":"WEKO"}]}]},"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":"naltr00280.pdf","filesize":[{"value":"3.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00280.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44523/files/naltr00280.pdf"},"version_id":"be00109a-95ab-43d3-993b-b28fe154cd8c"}]},"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":"ガン・タンネルによる鈍頭円錐の極超音速空力特性実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ガン・タンネルによる鈍頭円錐の極超音速空力特性実験"}]},"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":"44523","relation_version_is_last":true,"title":["ガン・タンネルによる鈍頭円錐の極超音速空力特性実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:55:35.766169+00:00"}