{"created":"2021-03-01T06:18:55.758584+00:00","id":11999,"links":{},"metadata":{"_buckets":{"deposit":"675c4757-7942-4db9-bf90-73e92b24853a"},"_deposit":{"id":"11999","owners":[],"pid":{"revision_id":0,"type":"depid","value":"11999"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00011999","sets":["320:321:322"]},"author_link":["37998","37999","38000","38001","38002","38003","38004","38005","38006","38007","38008","38009"],"item_10_alternative_title_19":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Effects of TSTO Orbiter Configuration on Supersonic Flow Field with Aerodynamic Interactions","subitem_alternative_title_language":"en"}]},"item_10_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-11-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"646","bibliographicPageEnd":"515","bibliographicPageStart":"509","bibliographicVolumeNumber":"55","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":"Supersonic flow fields around Two-Stage-To-Orbit (TSTO) models with different configurations have been experimentally examined in this paper. Four configurations for the orbiter have been considered: A) a hemisphere-cylinder, B) a hemisphere-cylinder with a flat bottom, C) an obliquely truncated circular cylinder, and D) a cone-cylinder. All the flow fields around these models showed complicated shock/shock and shock/boundary-layer interactions, which can be categorized into three patterns, depending on the extent to which the separation shock wave contributes to these interactions. The models B, C and D were proposed to suppress the pressure rise due to the interactions observed in the model A. As a result, the model B showed almost the same interactions as the model A, while in the model C they did not present. In the model D, a large pressure rise was seen in the case with no clearance, whereas the model undergoes the least aerodynamic interaction at a rather large clearance. It is concluded from these results that the model C is less affected by aerodynamic interactions due to the clearance than the other models.","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/2237/13875"}]},"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":"北村, 圭一","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"37998","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KITAMURA, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"37999","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"森, 浩一","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38000","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"MORI, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38001","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"花井, 勝祥","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38002","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"HANAI, Katsuhisa","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38003","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"矢橋, 務","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38004","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"YABASHI, Tsutomu","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38005","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"小澤, 啓伺","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38006","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"OZAWA, Hiroshi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38007","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 佳朗","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38008","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"NAKAMURA, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38009","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_v55_n646.pdf","filesize":[{"value":"1.3 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"jjsass_v55_n646.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/11999/files/jjsass_v55_n646.pdf"},"version_id":"25d45534-aeaa-4b57-a8e0-e461d803ff4c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"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":"TSTOオービタ形状の超音速空力干渉流れ場への影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"TSTOオービタ形状の超音速空力干渉流れ場への影響","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":"11999","relation_version_is_last":true,"title":["TSTOオービタ形状の超音速空力干渉流れ場への影響"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T03:58:24.721168+00:00"}