{"_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": ["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", "download_preview_message": "", "file_order": 0, "filename": "jjsass_v53_n622.pdf", "filesize": [{"value": "1.7 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_note", "mimetype": "application/pdf", "size": 1700000.0, "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"], "permalink_uri": "http://hdl.handle.net/2237/13879", "pubdate": {"attribute_name": "PubDate", "attribute_value": "2010-07-27"}, "publish_date": "2010-07-27", "publish_status": "0", "recid": "12003", "relation": {}, "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_shared_id": -1}