{"created":"2021-03-01T06:18:56.072860+00:00","id":12004,"links":{},"metadata":{"_buckets":{"deposit":"9ce26b17-bc05-47a5-bc5a-d258fb00e96f"},"_deposit":{"id":"12004","owners":[],"pid":{"revision_id":0,"type":"depid","value":"12004"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00012004","sets":["320:321:322"]},"author_link":["38031","38032","38033","38034","38035","38036"],"item_10_alternative_title_19":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Interaction between Delta Wing and Hemisphere-Cylinder in Supersonic Flow","subitem_alternative_title_language":"en"}]},"item_10_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-10-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"621","bibliographicPageEnd":"451","bibliographicPageStart":"446","bibliographicVolumeNumber":"53","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会論文集","bibliographic_titleLang":"ja"}]}]},"item_10_description_4":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"As future space vehicles, Reusable Launch Vehicle (RLV) needs to be developed, where there are two kinds of RLV: Single Stage To Orbit (SSTO) and Two Stage To Orbit (TSTO). In the latter case, the shock/shock interaction and shock/boundary layer interaction play a key role. In the present study, we focus on the supersonic flow field with aerodynamic interaction between a delta wing and a hemisphere-cylinder, which imitate a TSTO, where the clearance, h, between the delta wing and hemisphere-cylinder is a key parameter. As a result, complicated flow patterns were made clear, including separation bubbles.","subitem_description_language":"en","subitem_description_type":"Abstract"}]},"item_10_identifier_60":{"attribute_name":"URI","attribute_value_mlt":[{"subitem_identifier_type":"HDL","subitem_identifier_uri":"http://hdl.handle.net/2237/13880"}]},"item_10_publisher_32":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会","subitem_publisher_language":"ja"}]},"item_10_select_15":{"attribute_name":"著者版フラグ","attribute_value_mlt":[{"subitem_select_item":"publisher"}]},"item_10_source_id_7":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1344-6460","subitem_source_identifier_type":"PISSN"}]},"item_10_text_14":{"attribute_name":"フォーマット","attribute_value_mlt":[{"subitem_text_value":"application/pdf"}]},"item_1615787544753":{"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_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":"西野, 敦洋","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38031","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"NISHINO, Atsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38032","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"石川, 尊史","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38033","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"ISHIKAWA, Takahumi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38034","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 佳朗","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38035","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"NAKAMURA, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38036","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":"2018-02-20"}],"displaytype":"detail","filename":"jjsass_v53_n621.pdf","filesize":[{"value":"1.4 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"jjsass_v53_n621.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/12004/files/jjsass_v53_n621.pdf"},"version_id":"a4506a29-18be-4b78-8c2d-1b926f469b17"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Two Stage To Orbit (TSTO)","subitem_subject_scheme":"Other"},{"subitem_subject":"Supersonic Flow","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock/Shock Interaction","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock/Boundary-Layer Interaction","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":"超音速におけるデルタ翼・半球円柱間の空力干渉流れ場","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速におけるデルタ翼・半球円柱間の空力干渉流れ場","subitem_title_language":"ja"}]},"item_type_id":"10","owner":"1","path":["322"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2010-07-27"},"publish_date":"2010-07-27","publish_status":"0","recid":"12004","relation_version_is_last":true,"title":["超音速におけるデルタ翼・半球円柱間の空力干渉流れ場"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T03:58:39.004470+00:00"}