{"created":"2023-06-20T15:13:34.676190+00:00","id":43501,"links":{},"metadata":{"_buckets":{"deposit":"ee059004-a466-471b-b2dd-f612733cb01f"},"_deposit":{"created_by":1,"id":"43501","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43501"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043501","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463935","463934","463932","463933","463931","463936"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Simulations of Hypersonic Rarefied Transition-Regime Flows -DSMC Method and Navier-Stokes Computation-"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"32","bibliographicPageStart":"27","bibliographicVolumeNumber":"16","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory SP-16","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical solutions of the direct-simulation Monte Carlo (DSMC) method and the Navier-Stokes equation with a no-slip or a slip wall boundary condition are obtained for hypersonic rarefied monatomic gas flows in the transition regime (kn=0.1 - 0.001) around a finite-length parallel flat plate and a circular cylinder. A comparison among these numerical solutions indicates that the DSMC method is well applied to a fully continuum flow regime and the Navier-Stokes equation is applicable to the transition flow regime by the use of the slip wall boundary condition.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0016005","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 SP-16","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":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"日産自動車株式会社"},{"subitem_text_value":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Nissan Motor Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"嶋田, 徹"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和田, 安弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"古浦, 勝久"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Shimada, Toru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wada, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koura, Katsuhisa","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":"nalsp0016005.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0016005.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43501/files/nalsp0016005.pdf"},"version_id":"39000706-6aad-4d27-a7c5-564e1d8e11b8"}]},"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":"遷移領城流れのシミュレーション: DSMC法とNavier: Stokes数値解法","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"遷移領城流れのシミュレーション: DSMC法とNavier: Stokes数値解法"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43501","relation_version_is_last":true,"title":["遷移領城流れのシミュレーション: DSMC法とNavier: Stokes数値解法"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:13:17.616911+00:00"}