{"_buckets": {"deposit": "639ebab0-b1d5-4099-88d9-25c0b456192e"}, "_deposit": {"id": "11995", "owners": [], "pid": {"revision_id": 0, "type": "depid", "value": "11995"}, "status": "published"}, "_oai": {"id": "oai:nagoya.repo.nii.ac.jp:00011995", "sets": ["322"]}, "author_link": ["37972", "37973", "37974", "37975"], "item_10_alternative_title_19": {"attribute_name": "その他のタイトル", "attribute_value_mlt": [{"subitem_alternative_title": "Numerical Analysis on Aerodynamic Heating in Hypersonic Shock Interacting Flow", "subitem_alternative_title_language": "en"}]}, "item_10_biblio_info_6": {"attribute_name": "書誌情報", "attribute_value_mlt": [{"bibliographicIssueDates": {"bibliographicIssueDate": "2008-06-05", "bibliographicIssueDateType": "Issued"}, "bibliographicIssueNumber": "653", "bibliographicPageEnd": "277", "bibliographicPageStart": "269", "bibliographicVolumeNumber": "56", "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": "It is still challenging to predict surface heat-transfer rate in hypersonic flow computations. In this paper, we first performed numerical experiments by changing numerical flux functions and meshes for a hypersonic flow around a hemisphere. Results show that AUSM+ flux function by Liou (1996) on a carefully refined mesh can lead to a shock stable solution with an accurate aerodynamic heating on the surface. Then, a numerical simulation on a hypersonic flow around two bodies involving a shock/shock interaction and a boundary-layer separation has been conducted by using the same method. Although this is a rather difficult problem with a complicated flowfield, comparisons show good agreement with the corresponding experimental data, including the surface heat-transfer rate profile. Therefore, we can say that we have established a numerical method to accurately predict surface heat-transfer in hypersonic shock interacting flows. Finally, detailed analysis of the computed flowfield has been made.", "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/2237/13871"}]}, "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": "37972", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "KITAMURA, Keiichi", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "37973", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "中村, 佳朗", "creatorNameLang": "ja"}], "nameIdentifiers": [{"nameIdentifier": "37974", "nameIdentifierScheme": "WEKO"}]}, {"creatorNames": [{"creatorName": "NAKAMURA, Yoshiaki", "creatorNameLang": "en"}], "nameIdentifiers": [{"nameIdentifier": "37975", "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_v56_n653_p269.pdf", "filesize": [{"value": "1.8 MB"}], "format": "application/pdf", "future_date_message": "", "is_thumbnail": false, "licensetype": "license_note", "mimetype": "application/pdf", "size": 1800000.0, "url": {"label": "jjsass_v56_n653_p269.pdf", "objectType": "fulltext", "url": "https://nagoya.repo.nii.ac.jp/record/11995/files/jjsass_v56_n653_p269.pdf"}, "version_id": "825bd524-e7e6-4fa0-9dd2-c96dbfcfe535"}]}, "item_keyword": {"attribute_name": "キーワード", "attribute_value_mlt": [{"subitem_subject": "CFD", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Hypersonic Flow", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Shock Instability", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Heat Flux", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Shock/Shock Interaction", "subitem_subject_scheme": "Other"}, {"subitem_subject": "Boundary-Layer Separaion", "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": "極超音速衝撃波干渉流れにおける空力加熱の数値解析", "item_titles": {"attribute_name": "タイトル", "attribute_value_mlt": [{"subitem_title": "極超音速衝撃波干渉流れにおける空力加熱の数値解析", "subitem_title_language": "ja"}]}, "item_type_id": "10", "owner": "1", "path": ["322"], "permalink_uri": "http://hdl.handle.net/2237/13871", "pubdate": {"attribute_name": "PubDate", "attribute_value": "2010-07-27"}, "publish_date": "2010-07-27", "publish_status": "0", "recid": "11995", "relation": {}, "relation_version_is_last": true, "title": ["極超音速衝撃波干渉流れにおける空力加熱の数値解析"], "weko_shared_id": -1}