{"created":"2023-06-20T15:13:36.493211+00:00","id":43535,"links":{},"metadata":{"_buckets":{"deposit":"85e7e9c2-3869-48f3-804c-4b762e5473b3"},"_deposit":{"created_by":1,"id":"43535","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"43535"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00043535","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["464119","464125","464122","464123","464126","464124","464121","464128","464127","464120"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Heating Analysis for Axisymmetric Bodies in Supersonic Flow"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1991-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"250","bibliographicPageStart":"245","bibliographicVolumeNumber":"16","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory SP-16","bibliographic_titleLang":"en"}]}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Aerodynamic heating analyses have been performed for axisymmetric bodies in the supersonic flow. both experiments using a shock tunnel and the computations corresponding to the experiments are conducted. Heat flux to the bodies such as a hemisphere-cylinder and an ogive-cylinder are measured. Flow conditions are (1) Mach number M infinity = 4.25 (2) Reynolds numbers Re infinity = 2 - 3x105, based on body radius (3) Stagnation temperatures T0 = 500 - 600K (4) Angle of attack alpha = 0 degrees Results of the experiments and the computations are summarized as follows. Heat flux to the hemisphere surface has the maximum value at the stagnation point and decreases smoothly downstream. Also the heat flux to the ogive surface is quite large in the vicinity of the tip and decreases gradually downstream in the case of fully laminar or fully turbulent flow. In the case of the flow including the transition, increase of heat flux caused by the transition of the boundary layer is observed. LU-ADI difference scheme for compressible Navier-Stokes Code has been used for the computations corresponding to the experiments. Computational results show good correlation to the experimental data obtained by the shock tunnel.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: NALSP0016039","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-16","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory(NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱電機株式会社鎌倉製作所"},{"subitem_text_value":"三菱電機株式会社鎌倉製作所"},{"subitem_text_value":"三菱電機株式会社鎌倉製作所"},{"subitem_text_value":"九州大学工学部"},{"subitem_text_value":"三菱スペースソフトウェア株式会社"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Electric Corporation"},{"subitem_text_language":"en","subitem_text_value":"Kyushu University"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Space Software Corporation"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"片山, 雅之"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"黒崎, 隆二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中村, 淑子"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"麻生, 茂"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"熊坂, 和広"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Katayama, Masayuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kurosaki, Ryujiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamura, Yoshiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Aso, Shigeru","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kumasaka, Kazuhiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_files":{"attribute_name":"ファイル情報","attribute_type":"file","attribute_value_mlt":[{"accessrole":"open_date","date":[{"dateType":"Available","dateValue":"2020-01-28"}],"displaytype":"detail","filename":"nalsp0016039.pdf","filesize":[{"value":"479.0 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0016039.pdf","url":"https://jaxa.repo.nii.ac.jp/record/43535/files/nalsp0016039.pdf"},"version_id":"479e6ed9-2723-4dd4-82c8-b9f65f64b83e"}]},"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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"超音速飛しょう体頭部形状まわりの空力加熱解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"超音速飛しょう体頭部形状まわりの空力加熱解析"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"43535","relation_version_is_last":true,"title":["超音速飛しょう体頭部形状まわりの空力加熱解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T22:12:26.624694+00:00"}