{"created":"2023-06-20T15:13:31.565005+00:00","id":43446,"links":{},"metadata":{"_buckets":{"deposit":"a1c0cb54-c650-4267-a7b3-4a1c95ef9ec8"},"_deposit":{"created_by":1,"id":"43446","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43446"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043446","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["463689","463687","463690","463685","463686","463688"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Finite Difference Numerical Prediction of Aerodynamics for Airfoil Flying Over Wavy Wall"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1990-11","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"90","bibliographicPageStart":"83","bibliographicVolumeNumber":"14","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-14","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The lift on an airfoil flying over a wavy wall surface is calculated using a finite difference method, which was developed by J. Nakamichi1) to improve LTRAN2 evolved by W.F. Ballhaus & P.M. Goorjian2). Numerical computations include cases of a flat plate over a flat solid wall prior to the cases of a moving wavy wall. Modification of grid generating system is the major point for applying Nakamichi's method to our problem. The weak compressibility (M infinity =0.1-0.3) is considered but non-linearity is neglected in our calculations. The calculated results are compared with those obtained by the lifting surface theory of M. Ichikawa et al.3) The agreements are quite satisfactory.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0014013","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-14","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":"名古屋大学工学部航空学研究室"},{"subitem_text_value":"名古屋大学工学部航空学研究室"},{"subitem_text_value":"三菱重工業株式会社名古屋航空宇宙システム製作所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering, Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Department of Aeronautical Engineering, Nagoya University"},{"subitem_text_language":"en","subitem_text_value":"Aircraft Engineering Department Nagoya Aerospace Systems Mitsubishi Heavy Industries Ltd."}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"新田, 恭子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"安東, 茂典"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"和久, 浩行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nitta, Kyoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ando, Shigenori","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Waku, Hiroshi","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":"nalsp0014013.pdf","filesize":[{"value":"513.1 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0014013.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43446/files/nalsp0014013.pdf"},"version_id":"15092588-c576-4b3d-b39a-fc21498d5432"}]},"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":"波状壁面上を飛ぶ2次元翼空力荷重の差分法による計算","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"波状壁面上を飛ぶ2次元翼空力荷重の差分法による計算"}]},"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":"43446","relation_version_is_last":true,"title":["波状壁面上を飛ぶ2次元翼空力荷重の差分法による計算"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:14:34.306523+00:00"}