{"created":"2023-06-20T15:13:23.375731+00:00","id":43324,"links":{},"metadata":{"_buckets":{"deposit":"36141257-6ef3-42de-8e2c-d4ff073314e3"},"_deposit":{"created_by":1,"id":"43324","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43324"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043324","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463209","463208","463207","463210"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical Simulation of Flow Around the Aircraft Designed to Utilize Ground Effect"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1988-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"228","bibliographicPageStart":"223","bibliographicVolumeNumber":"9","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-9","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flow around an aircraft spatially designed to taking advantage of ground effect effectively is studied by using the incompressible Navier-Stokes equations. Third-order upwind difference scheme is used to solve the equations. Calculations are carried out under many conditions, i.e. the distance from the body to the ground, the angle of attack and the Reynolds number, etc. are changed systematically in order to investigate these effects on the flow field and force acting on the body.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0009033","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-9","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":"鳥取大学工学部"},{"subitem_text_value":"鳥取大学工学部"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Applied Mathematics and Physics, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Applied Mathematics and Physics, Tottori University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"河村, 哲也"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"久保, 昇三"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawamura, Tetsuya","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kubo, Shozo","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":"nalsp0009033.pdf","filesize":[{"value":"442.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0009033.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43324/files/nalsp0009033.pdf"},"version_id":"062d48c5-c062-43d6-a1d6-bb0a6522dedd"}]},"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":"地面効果翼機まわりの流れの数値シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"地面効果翼機まわりの流れの数値シミュレーション"}]},"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":"43324","relation_version_is_last":true,"title":["地面効果翼機まわりの流れの数値シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:17:24.236471+00:00"}