{"created":"2023-06-20T15:14:54.958694+00:00","id":44930,"links":{},"metadata":{"_buckets":{"deposit":"ab89464b-db50-4364-8169-5af0b04f893a"},"_deposit":{"created_by":1,"id":"44930","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"44930"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00044930","sets":["1887:1893","1896:1898:1913:1917"]},"author_link":["472016","472013","472014","472010","472011","472009","472015","472012"],"item_3_alternative_title_1":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"完全ポテンシャル流の遷音速翼型設計Ⅱ.汎用プログラムの開発"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1981-05","bibliographicIssueDateType":"Issued"},"bibliographicPageStart":"95","bibliographicVolumeNumber":"673","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所報告"},{"bibliographic_title":"Technical Report of National Aerospace Laboratory TR-673","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The Purpose of Part II of the paper is to present a user’s manual for the FORTRAN program which is coded following the numerical procedure developed for design of transonic airfoils. This procedure, described in Part I, has the following characteristics: 1)It can solve the inverse problem irrespective of the presence of shock waves. 2)The airfoil geometry is designed so that the width of the trailing edge is the required one. 3)The boundary layer calculation is included in this procedure: An actual airfoil geometry is obtained by subtracting a displacement thickness of a boundary layer from an airfoil geometry.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALTR0673000","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 TR-673","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":"0389-4010","subitem_source_identifier_type":"ISSN"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空宇宙技術研究所計算センター"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所空気力学第二部"},{"subitem_text_value":"航空宇宙技術研究所計算センター"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Second Aerodynamics Division, National Aerospace Laboratory(NAL)"},{"subitem_text_language":"en","subitem_text_value":"Computer Center, National Aerospace Laboratory(NAL)"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 登美子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"神谷, 信彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"河合, 伸坦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"小口, 慶子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"ISHIGURO, Tomiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAMIYA, Nobuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"KAWAI, Nobuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"OGUCHI, Keiko","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":"2020-01-29"}],"displaytype":"detail","filename":"naltr00673.pdf","filesize":[{"value":"5.2 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"naltr00673.pdf","url":"https://jaxa.repo.nii.ac.jp/record/44930/files/naltr00673.pdf"},"version_id":"d723b076-21a2-4414-bfab-b915f95d9e91"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"Transonic Airfoil Design of Full Potential Flow II. Development of the FORTRAN Code","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Transonic Airfoil Design of Full Potential Flow II. Development of the FORTRAN Code","subitem_title_language":"en"}]},"item_type_id":"3","owner":"1","path":["1893","1917"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"44930","relation_version_is_last":true,"title":["Transonic Airfoil Design of Full Potential Flow II. Development of the FORTRAN Code"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:48:19.556904+00:00"}