{"created":"2021-03-01T06:18:56.009951+00:00","id":12003,"links":{},"metadata":{"_buckets":{"deposit":"ac49f656-969e-439b-8a20-f628f901194f"},"_deposit":{"id":"12003","owners":[],"pid":{"revision_id":0,"type":"depid","value":"12003"},"status":"published"},"_oai":{"id":"oai:nagoya.repo.nii.ac.jp:00012003","sets":["320:321:322"]},"author_link":["38023","38024","38025","38026","38027","38028","38029","38030"],"item_10_alternative_title_19":{"attribute_name":"その他のタイトル","attribute_value_mlt":[{"subitem_alternative_title":"Effect of the Clearance between Two Bodies on TSTO Aerodynamic Heatin","subitem_alternative_title_language":"en"}]},"item_10_biblio_info_6":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-11-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"622","bibliographicPageEnd":"509","bibliographicPageStart":"503","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":"TSTO (Two Stage To Orbit) is a candidate for advanced space transportation system, which is required to fly over a wide region from subsonic to hypersonic speed with an orbiter connected with a booster. The hypersonic flow field with aerodynamic interaction around a TSTO model, which consists of a delta wing as a booster and a hemisphere-cylinder as an orbiter, has been investigated. The temperature distribution is measured by the Temperature Sensitive Paint (TSP) method, and the heat flux with thermo-couples. As a result, the flow field has been significantly affected by the clearance between the two bodies. In the case of a small clearance, heat flux on the head of the hemisphere-cylinder becomes about 3.1 times as large as the stagnation heat flux for the hemisphere-cylinder alone. On the other hand, at a large clearance, heat flux on the delta wing becomes about 1.1 times as large as the stagnation heat flux. In addition, a new thermal protection system (TPS) to reduce the aerodynamic heating due to shock/shock interaction and shock/boundary-layer interaction is also investigated in this paper. A triangular prism installed on the delta wing can change the aerodynamic heating, depending on its location. It was found that a small device installed upstream is effective, where the heat flux has been reduced by about 48%.","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/2237/13879"}]},"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":"38023","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"NISHINO, Atsuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38024","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"石川, 尊史","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38025","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"ISHIKAWA, Takahumi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38026","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"北村, 圭一","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38027","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"KITAMURA, Keiichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38028","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"中村, 佳朗","creatorNameLang":"ja"}],"nameIdentifiers":[{"nameIdentifier":"38029","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"NAKAMURA, Yoshiaki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"38030","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_n622.pdf","filesize":[{"value":"1.7 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"jjsass_v53_n622.pdf","objectType":"fulltext","url":"https://nagoya.repo.nii.ac.jp/record/12003/files/jjsass_v53_n622.pdf"},"version_id":"9fa6f9e5-afb7-442e-b333-9f2be957984e"}]},"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":"Hypersonic Flow","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock/Shock Interaction","subitem_subject_scheme":"Other"},{"subitem_subject":"Shock/Boundary-Layer Interaction","subitem_subject_scheme":"Other"},{"subitem_subject":"Temperature Sensitive Paint (TSP)","subitem_subject_scheme":"Other"},{"subitem_subject":"Heat Flux","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":"極超音速TSTO空力干渉流れ場における2物体間隔の空力加熱率への影響","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"極超音速TSTO空力干渉流れ場における2物体間隔の空力加熱率への影響","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":"12003","relation_version_is_last":true,"title":["極超音速TSTO空力干渉流れ場における2物体間隔の空力加熱率への影響"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T03:58:38.972862+00:00"}