{"created":"2021-03-01T06:18:55.509724+00:00","id":11995,"links":{},"metadata":{"_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":["320:321:322"]},"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","filename":"jjsass_v56_n653_p269.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","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"],"pubdate":{"attribute_name":"PubDate","attribute_value":"2010-07-27"},"publish_date":"2010-07-27","publish_status":"0","recid":"11995","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_creator_id":"1","weko_shared_id":-1},"updated":"2023-01-16T03:58:36.294927+00:00"}