{"created":"2023-06-20T15:13:19.959286+00:00","id":43260,"links":{},"metadata":{"_buckets":{"deposit":"eec19743-fd90-478f-990b-786db3bdfa1a"},"_deposit":{"created_by":1,"id":"43260","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43260"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043260","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["462889","462890","462887","462885","462888","462886"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Navier-Stokes Analysis of Transonic Transport Aircraft Empennage"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1987-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"54","bibliographicPageStart":"49","bibliographicVolumeNumber":"8","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-8","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Flow field simulations over transonic transport aircraft empennage were carried out based on three-dimensional Navier-Stokes equations. The computations were done for the flow fields of various Mach numbers and angles of attack to investigate the variation of the lift curve slope with Mach number at low angle of attack, and the variation of the lift coefficient with angle of attack at low Mach number. The values of lift curve slope obtained by the computations show good agreement with those by experiments. While the difference between computations and experiments looks a little large about lift coefficient versus angle of attack.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0008007","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-8","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":"富士重工業株式会社"},{"subitem_text_value":"富士重工業株式会社"},{"subitem_text_value":"日本航空機開発協会"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd."},{"subitem_text_language":"en","subitem_text_value":"Japan Aircraft Development Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"越岡, 康弘"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"加茂, 圭介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"天野, 完一"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Koshioka, Yasuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kamo, Keisuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Amano, Kan-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":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0008007.pdf","filesize":[{"value":"428.4 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0008007.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43260/files/nalsp0008007.pdf"},"version_id":"4f3e47c6-a75c-443e-8ed9-c6b49bf452e4"}]},"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":"ナビェ・ストークス方程式による尾翼回りの流れの解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"ナビェ・ストークス方程式による尾翼回りの流れの解析"}]},"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":"43260","relation_version_is_last":true,"title":["ナビェ・ストークス方程式による尾翼回りの流れの解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:19:02.666293+00:00"}