{"created":"2023-06-20T15:13:14.409232+00:00","id":43167,"links":{},"metadata":{"_buckets":{"deposit":"6b2b8ccf-83e8-4b73-8c4a-226ab84b8f66"},"_deposit":{"created_by":1,"id":"43167","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43167"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043167","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462454","462451","462452","462453"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Solution of Viscous Compressible Flows Past an Airfoil Using Unconditionally Stable Explicit Method"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1984-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"212","bibliographicPageStart":"201","bibliographicVolumeNumber":"3","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-3","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"An unconditionally stable explicit method has been applied to compute compressible laminar flows past an NACA0012 airfoil. The method is based on a combination of central differencing for spatial derivatives with a rational Runge-Kutta time integration scheme. Both transonic (M","subitem_description_type":"Other"},{"subitem_description":"An unconditionally stable explicit method has been applied to compute compressible laminar flows past an NACA0012 airfoil. The method is based on a combination of central differencing for spatial derivatives with a rational Runge-Kutta time integration scheme. Both transonic (M = 0.8) and supersonic (M = 2.0) flow cases have been calculated for various Reynolds numbers. Physically plausible results are obtained for each case within practically feasible CPU time.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0003025","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-3","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":"京都工芸繊維大学工芸学部"},{"subitem_text_value":"京都工芸繊維大学工芸学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyoto Institute of Technology"},{"subitem_text_language":"en","subitem_text_value":"Kyoto Institute of Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"里深, 信行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"西田, 雄亮"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Satofuka, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nishida, Yuusuke","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":"nalsp0003025.pdf","filesize":[{"value":"802.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0003025.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43167/files/nalsp0003025.pdf"},"version_id":"99da50a9-e2b1-40e3-a27d-e87980a36c40"}]},"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":"無条件安定な陽的差分法による翼型まわりの粘性流の解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"無条件安定な陽的差分法による翼型まわりの粘性流の解析"}]},"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":"43167","relation_version_is_last":true,"title":["無条件安定な陽的差分法による翼型まわりの粘性流の解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:21:16.609656+00:00"}