{"created":"2023-06-20T14:53:34.994507+00:00","id":21783,"links":{},"metadata":{"_buckets":{"deposit":"e9ff90f9-ff72-44b0-a770-1b022395b6aa"},"_deposit":{"created_by":1,"id":"21783","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"21783"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00021783","sets":["1887:1888"]},"author_link":["204464","204462","204465","204467","204468","204469","204463","204466"],"item_7_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aerodynamic Heating Analysis for Inflatable Reentry Vehicle"}]},"item_7_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2017-12-05","bibliographicIssueDateType":"Issued"},"bibliographicIssueNumber":"12","bibliographicPageEnd":"376(18)","bibliographicPageStart":"370(12)","bibliographicVolumeNumber":"65","bibliographic_titles":[{"bibliographic_title":"日本航空宇宙学会誌"},{"bibliographic_title":"Aeronautical and Space Sciences Japan","bibliographic_titleLang":"en"}]}]},"item_7_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"極超音速領域における柔軟構造再突入機の空力加熱が実験的・解析的に調べられた. 実験装置としてJAXA極超音速風洞, 数値解析ソルバーとしてFaSTAR/RG-FaSTARが用いられている. 風洞試験において, いくつかの迎角のケースに対して, シュリーレン画像による密度勾配分布と赤外線サーモグラフィによる表面熱流束が計測された. これらの計測結果に基づき解析モデルの検証が合わせて実施され, 空力加熱に対して良好な予測性能が確認された. 低迎角ケースでは, 衝撃層の形成とそれによる表面熱流束の増加, 背面における強い膨張波の形成が確認された. 大きな迎角での特徴的な現象として, 模型頭頂部の剥離による渦の形成と, 対応する模型表面での熱流束低下が認められた. 今回の実験結果および解析結果より, 衝撃層における流れ場は乱流ではないと推察されるが, 剥離後の領域は乱流場であることが示唆された.","subitem_description_type":"Abstract"}]},"item_7_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: 図版あり","subitem_description_type":"Other"}]},"item_7_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains illustrations","subitem_description_type":"Other"}]},"item_7_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: DS1740337003","subitem_description_type":"Other"}]},"item_7_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"Japan Society for Aeronautical and Space Sciences"}]},"item_7_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"日本航空宇宙学会"}]},"item_7_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0021-4663","subitem_source_identifier_type":"ISSN"}]},"item_7_source_id_24":{"attribute_name":"書誌レコードID","attribute_value_mlt":[{"subitem_source_identifier":"AN00189072","subitem_source_identifier_type":"NCID"}]},"item_access_right":{"attribute_name":"アクセス権","attribute_value_mlt":[{"subitem_access_right":"metadata only access","subitem_access_right_uri":"http://purl.org/coar/access_right/c_14cb"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"高橋, 裕介"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"松永, 学"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"大島, 伸行"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"山田, 和彦"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Takahashi, Yusuke","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Matsunaga, Manabu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oshima, Nobuyuki","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Yamada, Kazuhiko","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"Inflatable Reentry Vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Hypersonic Flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Aerodynamic Heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Numerical Analysis","subitem_subject_language":"en","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":"柔軟エアロシェル大気圏突入機の空力加熱解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"柔軟エアロシェル大気圏突入機の空力加熱解析"}]},"item_type_id":"7","owner":"1","path":["1888"],"pubdate":{"attribute_name":"公開日","attribute_value":"2018-01-09"},"publish_date":"2018-01-09","publish_status":"0","recid":"21783","relation_version_is_last":true,"title":["柔軟エアロシェル大気圏突入機の空力加熱解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T03:30:49.151690+00:00"}