{"created":"2023-06-20T14:37:42.944645+00:00","id":4133,"links":{},"metadata":{"_buckets":{"deposit":"29be1929-e49e-4820-ae38-c3830742af0f"},"_deposit":{"created_by":1,"id":"4133","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"4133"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00004133","sets":["1887:1891","9:789:868:887"]},"author_link":["17803","17810","17808","17806","17811","17809","17802","17805","17804","17807"],"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2013-11-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"315","bibliographicPageStart":"307","bibliographicVolumeNumber":"JAXA-SP-13-001E","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料"},{"bibliographic_title":"JAXA Special Publication","bibliographic_titleLang":"en"}]}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan","subitem_description_type":"Other"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"In this study, shock layer radiation is investigated by experimental and numerical approach. Radiation profiles of N2, N2(+), and N are observed in two test conditions of initial pressure and velocity by time-resolved emission spectroscopy. Flow properties behind shock front are computed by the CFD code with two-temperature thermochemical model. The results are used as inputs for the radiation analysis code “SPRADIAN 2” to derive the radiation profiles behind shock front along the line of sight. Comparison between experiments and calculations shows that the decline of calculated radiation intensity is slower than that of measured one.Therefore, the present calculation fails to reproduce the measured radiation profile. This is considered to be due to the fact that the two-temperature model seems to lose its accuracy in the intermediate hypersonic flow regime. Further investigations are necessary to improve the accuracy of the two-temperature model.","subitem_description_type":"Other"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color illustrations","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0062070025","subitem_description_type":"Other"}]},"item_5_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: JAXA-SP-13-001E","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙航空研究開発機構(JAXA)"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Japan Aerospace Exploration Agency (JAXA)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"1349-113X","subitem_source_identifier_type":"ISSN"}]},"item_5_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AA11984031","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"},{"subitem_text_value":"鳥取大学大学院工学研究科機械宇宙工学専攻"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"},{"subitem_text_language":"en","subitem_text_value":"Department of Mechanical and Aerospace Engineering, Graduate School of Engineering, Tottori University"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"山田, 剛治"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"吾郷, 祥太"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"久保, 優斗"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松野, 隆"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"川添, 博光"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Gouji","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ago, Shota","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kubo, Yuto","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsuno, Takashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kawazoe, Hiromitsu","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":"2020-01-16"}],"displaytype":"detail","filename":"62070025.pdf","filesize":[{"value":"233.2 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"62070025.pdf","url":"https://jaxa.repo.nii.ac.jp/record/4133/files/62070025.pdf"},"version_id":"334d2817-5e19-4e85-a532-d0fb23d594eb"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"shock tube","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock layer radiation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermochemical nonequilibrium","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spectroscopy","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"planetary entry","subitem_subject_language":"en","subitem_subject_scheme":"Other"}]},"item_language":{"attribute_name":"言語","attribute_value_mlt":[{"subitem_language":"eng"}]},"item_resource_type":{"attribute_name":"資源タイプ","attribute_value_mlt":[{"resourcetype":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"Experimental and Numerical Study on Shock Layer Radiation for Planetary Entry Flights","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"Experimental and Numerical Study on Shock Layer Radiation for Planetary Entry Flights","subitem_title_language":"en"}]},"item_type_id":"5","owner":"1","path":["887","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"4133","relation_version_is_last":true,"title":["Experimental and Numerical Study on Shock Layer Radiation for Planetary Entry Flights"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:46:43.681060+00:00"}