{"created":"2023-06-20T14:54:18.331006+00:00","id":22620,"links":{},"metadata":{"_buckets":{"deposit":"c2433dce-1286-40bb-be6e-98a557131b2f"},"_deposit":{"created_by":1,"id":"22620","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"22620"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00022620","sets":["1887:1888"]},"author_link":["211847","211845","211842","211843","211844","211846"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Supersonic Natural Laminar Flow Effect on Axisymmetric Bodies with Sinusoidal Deformation"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2014-08-28","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"59","bibliographicPageStart":"55","bibliographicVolumeNumber":"13","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術"}]}]},"item_7_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The transition characteristics on candidate shapes were examined numerically and experimentally in order to design a natural laminar flow fuselage nose for supersonic transport. The candidate shapes were designed through axisymmetric sinusoidal deformations added on base shapes. Not only parameters of geometry which define the deformation, but also the conditions of uniform flow were varied to obtain the greatest effect of natural laminar flow. From the results, the natural laminar flow effect was found to be obtained in cases of the small ratio of pressure gradients in azimuthal and axial directions in the side area. The natural laminar flow effect was validated experimentally.","subitem_description_type":"Other"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: PA1520035000","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Japan Society for Aeronautical and Space Sciences"}]},"item_7_relation_25":{"attribute_name":"DOI","attribute_value_mlt":[{"subitem_relation_name":[{"subitem_relation_name_text":"info:doi/10.2322/astj.13.55"}],"subitem_relation_type_id":{"subitem_relation_type_id_text":"http://dx.doi.org/10.2322/astj.13.55","subitem_relation_type_select":"DOI"}}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1884-0477","subitem_source_identifier_type":"ISSN"}]},"item_7_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"宇宙航空研究開発機構航空本部（JAXA）"},{"subitem_text_value":"株式会社TOUA"},{"subitem_text_value":"東京ビジネスサービス株式会社"}]},"item_7_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Institute of Aeronautical Technology, Japan Aerospace Exploration Agency (JAXA)"},{"subitem_text_language":"en","subitem_text_value":"TOUA Corporation"},{"subitem_text_language":"en","subitem_text_value":"Tokyo Business Service Co. Ltd."}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"徳川, 直子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"石川, 敬掲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"上田, 良稲"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Tokugawa, Naoko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishikawa, Hiroaki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ueda, Yoshine","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Drag Reduction","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Boundary-layer Transition","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Natural Laminar Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Fuselage Nose","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"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":"journal article","resourceuri":"http://purl.org/coar/resource_type/c_6501"}]},"item_title":"正弦波変形による軸対称物体の超音速自然層流効果","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"正弦波変形による軸対称物体の超音速自然層流効果"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-08-17"},"publish_date":"2015-08-17","publish_status":"0","recid":"22620","relation_version_is_last":true,"title":["正弦波変形による軸対称物体の超音速自然層流効果"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:18:05.247362+00:00"}