{"created":"2023-06-20T15:02:27.912379+00:00","id":31546,"links":{},"metadata":{"_buckets":{"deposit":"bbdad334-dd7b-4592-b842-48fab2c1462f"},"_deposit":{"created_by":1,"id":"31546","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"31546"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00031546","sets":["1887:1890","1896:1898:1899:1910"]},"author_link":["404786","404791","404789","404788","404790","404787"],"item_9_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Supersonic Flow past Conical Bodies at Large Angles of Attack (1)"}]},"item_9_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1974-01","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"1_A","bibliographicPageEnd":"71","bibliographicPageStart":"62","bibliographicVolumeNumber":"10","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":"円錐が大きな迎角(相対迎角α/θ_0 > 1)をとるとき,非粘性超音速流れの中に,特異点が発生することは,よく知られている.本報告は下半分(風上側)に円錐,上半分(風下側)に檜円錐という錐休を考え,それによって特元気の発生を防ぎ,その結果が,大迎角時の円錐回りの圧力分布をよく近似しうるということを示したものである.","subitem_description_type":"Abstract"}]},"item_9_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In the study of an inviscid supersonic flow past conical bodies at large angles of attack (relative incidence α/θ_0 > 1), one of the difficulties is the appearance of the vortical singularity in the flow field pointed out by Ferri. The phenomenon of the \"lift off\" of the vortical singularity causes the divergence of the computation of the conical flow field. In order to avoid the divergence, in this report we have proposed the method that varied a standard circular cone as follows; the windwardside shape leaves a circular cone as it is and the leeward-side shape is replaced by an elliptic cone, which is expanded gradually in proportion to the increase of the angle of attack as including the vortical singularity. By solving the flow field of this equivalent body and applying this results, we have attempted to approximate the pressure distribution of the standard circular cone at large angles of attack. The agreement between the results of the present method and the experiments is good.","subitem_description_type":"Other"}]},"item_9_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: SA0124469000","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"},{"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"},{"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":"玉木, 章夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河村, 龍馬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中尾, 晨一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"TAMAKI, Fumio","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAMURA, Ryuma","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"NAKAO, Shin-ichi","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":"2020-01-23"}],"displaytype":"detail","filename":"SA0124469.pdf","filesize":[{"value":"600.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"SA0124469.pdf","url":"https://jaxa.repo.nii.ac.jp/record/31546/files/SA0124469.pdf"},"version_id":"048c152b-21ee-4167-b81d-5a817aaa9433"}]},"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":"大きな迎角をもつ錐体を過ぎる流れの研究(1)","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"大きな迎角をもつ錐体を過ぎる流れの研究(1)"}]},"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":"31546","relation_version_is_last":true,"title":["大きな迎角をもつ錐体を過ぎる流れの研究(1)"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T00:57:00.877140+00:00"}