{"created":"2021-03-01T06:39:05.519243+00:00","id":30739,"links":{},"metadata":{"_buckets":{"deposit":"4cf9ac64-4355-48ba-8c59-54b321c9b699"},"_deposit":{"id":"30739","owners":[],"pid":{"revision_id":0,"type":"depid","value":"30739"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00030739","sets":["320:2524:2544:2551"]},"author_link":["101971","101972","101973"],"item_1615768549627":{"attribute_name":"出版タイプ","attribute_value_mlt":[{"subitem_version_resource":"http://purl.org/coar/version/c_970fb48d4fbd8a85","subitem_version_type":"VoR"}]},"item_9_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1989-03-31","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"2","bibliographicPageEnd":"350","bibliographicPageStart":"337","bibliographicVolumeNumber":"40","bibliographic_titles":[{"bibliographic_title":"Memoirs of the Faculty of Engineering, Nagoya University","bibliographic_titleLang":"en"}]}]},"item_9_description_5":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"A computer code based on the 1st order panel method is presented for solving inviscid incompressible flow fields about 3-D airplane-like bodies. A sample problem chosen for a test is solved and a comparison with other computational results shows good agreement. To increase the accuracy of the method, especially for a thin wing, the number of doublet panels on the camber surface of a wing is multiplied in the chordwise direction by a factor, which enhances the accuracy to some extent.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_9_identifier_registration":{"attribute_name":"ID登録","attribute_value_mlt":[{"subitem_identifier_reg_text":"10.18999/memfenu.40.2.337","subitem_identifier_reg_type":"JaLC"}]},"item_9_publisher_32":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Faculty of Engineering, Nagoya University","subitem_publisher_language":"en"}]},"item_9_select_15":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_select_item":"publisher"}]},"item_9_source_id_7":{"attribute_name":"ISSN（print）","attribute_value_mlt":[{"subitem_source_identifier":"0027-7657","subitem_source_identifier_type":"PISSN"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"open access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_abf2"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"Choi, Jang-Soo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"101971","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Chang, Keun-Shik","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"101972","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Sugiyama, Yoshiyuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"101973","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":"2020-10-29"}],"displaytype":"detail","filename":"40-2-05.pdf","filesize":[{"value":"911.9 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"40-2-05.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/30739/files/40-2-05.pdf"},"version_id":"4626645b-9bff-448d-88fd-2c8cb361ded2"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"departmental bulletin paper","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"An application of the surface-singularity method to wing-body-tail configurations","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"An application of the surface-singularity method to wing-body-tail configurations","subitem_title_language":"en"}]},"item_type_id":"9","owner":"1","path":["2551"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2020-10-29"},"publish_date":"2020-10-29","publish_status":"0","recid":"30739","relation_version_is_last":true,"title":["An application of the surface-singularity method to wing-body-tail configurations"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T05:13:22.793004+00:00"}