{"created":"2023-06-20T14:47:00.847873+00:00","id":14633,"links":{},"metadata":{"_buckets":{"deposit":"1dc5e89c-35ee-4c4e-9927-815b0b4740f9"},"_deposit":{"created_by":1,"id":"14633","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14633"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014633","sets":["1543:1656:1668","1887:1891"]},"author_link":["133729","133730","133731","133733","133728","133735","133734","133732"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical simulation on strong shock waves propagating in a two-dimensional nozzle"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2005-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"105","bibliographicPageStart":"102","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム　平成16年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics 2004","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"When a space vehicle returns into the earth atmosphere, the gas temperature around the vehicle becomes very high owing to mainly shock compression. To protect the vehicle from such high temperature environment, the problem on the aerodynamic heating should be analyzed precisely. In the present numerical computations, the high temperature air-flow with the real gas effects such as dissociation and ionization is studied to simulate hypersonic flows produced in a conical nozzle of the gun-tunnel placed at the Aoyama Gakuin University. The 2-D Euler code is used together with TVD scheme for shock discontinuity. To simulate the high temperature air-flow produced in a small hypersonic gun-tunnel located at Aoyama Gakuin University, numerical computations are performed by applying the 2-D Euler code with TVD scheme. The real gas effects of high temperature air with dissociation and ionization are taken into account.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0048089026","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宇宙科学研究本部"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"青山学院大学 大学院"},{"subitem_text_value":"青山学院大学 理工学部"},{"subitem_text_value":"青山学院大学 理工学部"},{"subitem_text_value":"東京農工大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Aoyama Gakuin University Graduate School"},{"subitem_text_language":"en","subitem_text_value":"Aoyama Gakuin University College of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Aoyama Gakuin University College of Science and Engineering"},{"subitem_text_language":"en","subitem_text_value":"Tokyo University of Agriculture and Technology Faculty of Engineering"}]},"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":"森田, 和貴"}],"nameIdentifiers":[{"nameIdentifier":"133728","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"古川, 信夫"}],"nameIdentifiers":[{"nameIdentifier":"133729","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"林, 光一"}],"nameIdentifiers":[{"nameIdentifier":"133730","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"東野, 文男"}],"nameIdentifiers":[{"nameIdentifier":"133731","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Morita, Kazuki","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"133732","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Furukawa, Nobuo","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"133733","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Hayashi, Koichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"133734","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Higashino, Fumio","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"133735","nameIdentifierScheme":"WEKO"}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"2次元流","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波伝播","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃圧縮","subitem_subject_scheme":"Other"},{"subitem_subject":"ノズル流","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"実在気体効果","subitem_subject_scheme":"Other"},{"subitem_subject":"two dimensional flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave propagation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock compression","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nozzle flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"real gas effect","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":"conference paper","resourceuri":"http://purl.org/coar/resource_type/c_5794"}]},"item_title":"2次元ノズル中を伝播する強い衝撃波背後の数値解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"2次元ノズル中を伝播する強い衝撃波背後の数値解析"}]},"item_type_id":"5","owner":"1","path":["1668","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14633","relation_version_is_last":true,"title":["2次元ノズル中を伝播する強い衝撃波背後の数値解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:31:43.247801+00:00"}