{"created":"2023-06-20T15:14:00.361045+00:00","id":43976,"links":{},"metadata":{"_buckets":{"deposit":"1333eca3-a9a6-46ba-9dc1-3d171e30352f"},"_deposit":{"created_by":1,"id":"43976","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43976"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043976","sets":["1887:1893","1896:1898:1913:1916"]},"author_link":["466817","466823","466825","466815","466821","466824","466819","466822","466826","466820","466818","466816"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic and Flow-Visualization Studies of Half-blunt Cones at Supersonic Speeds"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1979-09","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"42","bibliographicVolumeNumber":"393","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":"This paper presents the aerodynamic characteristics of some blunt half-cones with and without fins which have been considered typical configurations of lifting recovering-bodies,and the flow visualizations of leeward separation at angles of attack.The wind tunnel force tests were conducted over the Mach number range 1.5 to 3.0 and for angles of attack from -25° to 25°.The experimental results show that the aerodynamic hysteresis due to lee-surface separation was not observed and,CN and Cm against α were well predicted by slender body approximation better than by Newtonian approximation.The flow-visualizations of lee-surface separation were also conducted at low supersonic speeds.Visualization techniques consisted of the schlieren,oil flow and vapor screen methods.In the vapor screen photographs,two flow patterns over the leeside of a half-cone were observed according to attack angle.The first,at a 10° attack angle,had only a pair of vortex similar to incompressible flow cases.The second,at a 20° atthad a plane shock wave connected with a pair of vortexes.The lee-surface flow patterns were schematically depicted from these visualized pictures.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTM0393000","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-393","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"},{"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":"河本, 巖"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"清水, 福寿"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"外立, 政隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"野田, 順一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"関根, 英夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石田, 清道"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMOTO, Iwao","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SHIMIZU, Fukuju","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"HASHIDATE, Masataka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NODA, Jun-ichi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"SEKINE, Hideo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIDA, Kiyomichi","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":"naltm00393.pdf","filesize":[{"value":"4.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltm00393.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43976/files/naltm00393.pdf"},"version_id":"d3249cfb-4005-4018-8f5e-09ea2d37e036"}]},"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":"鈍頭半円錐物体の超音速空力特性とその背面剥離の可視化実験","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"鈍頭半円錐物体の超音速空力特性とその背面剥離の可視化実験"}]},"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":"43976","relation_version_is_last":true,"title":["鈍頭半円錐物体の超音速空力特性とその背面剥離の可視化実験"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:04:43.541976+00:00"}