{"created":"2023-06-20T14:47:03.941316+00:00","id":14690,"links":{},"metadata":{"_buckets":{"deposit":"65b9e198-1980-42d3-a840-f9c2a1b76fa1"},"_deposit":{"created_by":1,"id":"14690","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"14690"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00014690","sets":["1543:1656:1670","1887:1891"]},"author_link":["134158","134161","134159","134160"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Assessment of the two-temperature model for reentry flow simulations"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2003-03","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"12","bibliographicPageStart":"9","bibliographic_titles":[{"bibliographic_title":"宇宙航行の力学シンポジウム　平成14年度"},{"bibliographic_title":"Symposium on Flight Mechanics and Astrodynamics 2002","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The two-temperature model was assessed for simulating the chemically and thermally nonequilibrium flows around the reentry vehicle. In this analysis, the effect of the parameters for the model on the thickness of the shock layer and the stagnation point heat flux are compared. The flow condition is that the reentry speed is 8.0 km/s at the altitude of 60 km. It was found that the effect of parameters on the thermal nonequilibrium inside the shock layer is significant. But the shock stand-off distance, shock shape, and the heat flux are not affected significantly.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0045913003","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"宇宙科学研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"The Institute of Space and Astronautical Science (ISAS)"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"静岡大学 工学部"},{"subitem_text_value":"静岡大学 工学部"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Shizuoka University Faculty of Engineering"},{"subitem_text_language":"en","subitem_text_value":"Shizuoka University 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":"大津, 広敬"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"宮澤, 政文"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Otsu, Hirotaka","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Miyazawa, Masafumi","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"熱化学モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"2温度モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡流","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙機再突入","subitem_subject_scheme":"Other"},{"subitem_subject":"衝撃波","subitem_subject_scheme":"Other"},{"subitem_subject":"解離","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"研究開発","subitem_subject_scheme":"Other"},{"subitem_subject":"エネルギー緩和","subitem_subject_scheme":"Other"},{"subitem_subject":"電子温度","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"thermochemical model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"two-temperature model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"spacecraft reentry","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"shock wave","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"dissociation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic heating","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"research and development","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"energy relaxation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"electron temperature","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":"再突入飛行環境のシミュレーションに用いられる2温度モデルの検証","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"再突入飛行環境のシミュレーションに用いられる2温度モデルの検証"}]},"item_type_id":"5","owner":"1","path":["1670","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"14690","relation_version_is_last":true,"title":["再突入飛行環境のシミュレーションに用いられる2温度モデルの検証"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T05:30:52.451891+00:00"}