{"created":"2023-06-20T15:13:17.994254+00:00","id":43224,"links":{},"metadata":{"_buckets":{"deposit":"af1aa7d2-4a34-455e-9d4d-806889095413"},"_deposit":{"created_by":1,"id":"43224","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43224"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043224","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462690","462693","462694","462691","462695","462692"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Calculations of the Flowfield Around Propellers"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1986-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"70","bibliographicPageStart":"61","bibliographicVolumeNumber":"7","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-7","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In order to examine the flowfield around ATP by numerical calculations, the finite difference methods are applied. In the first part of this paper, the partial differential equation for the disturbance velocity potential is solved by the line relaxation technique. In order to do the calculations, boundary fitted meshes are generated. The transforma-tions between physical and computational space are performed by chain rule. The SR-3 is used for numerical calculations. In the second part of the paper, the Euler equations are solved by non-iterative implicit ADI schemes in AF alogrithm. Boundary fitted meshes are also used for this case. The results show qualitative agreement with the results obtained by Bober et al. Finally, the aerodynamic performances, such as power co-efficients and efficiencies, are obtained. Potential calculations show that these quantities are relative]y larger than the experimental values obtained by NASA; however, Euler solutions show that the values come closer to the experimental values.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0007008","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-7","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":"京都大学工学部航空"},{"subitem_text_value":"三菱重工"},{"subitem_text_value":"トヨタ自動車"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Kyoto University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Co. Ltd."},{"subitem_text_language":"en","subitem_text_value":"Toyota Motors"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"小早川, 命"}],"nameIdentifiers":[{"nameIdentifier":"462690","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小沼, 裕之"}],"nameIdentifiers":[{"nameIdentifier":"462691","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"塩田, 泰宏"}],"nameIdentifiers":[{"nameIdentifier":"462692","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kobayakawa, Makoto","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"462693","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Onuma, Hiroyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"462694","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Shiota, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"462695","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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0007008.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0007008.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43224/files/nalsp0007008.pdf"},"version_id":"9a410dd6-35c0-4d08-96b4-bd476fb757fd"}]},"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":"プロペラまわりの流れの数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"プロペラまわりの流れの数値解析"}]},"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":"43224","relation_version_is_last":true,"title":["プロペラまわりの流れの数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:19:54.756674+00:00"}