{"created":"2023-06-20T14:39:09.399605+00:00","id":5839,"links":{},"metadata":{"_buckets":{"deposit":"328055dc-cc94-4304-9d3a-9977837e6561"},"_deposit":{"created_by":1,"id":"5839","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"5839"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00005839","sets":["1887:1891","9:789:998:1014"]},"author_link":["28746","28745"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Air models used in the JAXA hypersonic wind tunnels"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2007-03-30","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"26","bibliographicPageStart":"23","bibliographicVolumeNumber":"JAXA-SP-06-020","bibliographic_titles":[{"bibliographic_title":"宇宙航空研究開発機構特別資料: 第76回風洞研究会議論文集"},{"bibliographic_title":"JAXA Special Publication: Proceedings of the Wind Tunnel Technology Association 76th Meeting","bibliographic_titleLang":"en"}]}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Three air models are used in JAXA hypersonic wind tunnel. They are 'perfect', 'thermally perfect', and 'real' models. Thermally perfect model considers an atomic-vibration energy. Real model considers an atomic vibration and an inter-molecular potential energy. The three models were comparatively investigated by program codes. It revealed that thermally perfect or real model has to be used in a precise analysis in hypersonic calculations.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0063330004","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-06-020","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"}]},"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":"宇宙航空研究開発機構 総合技術研究本部　風洞技術開発センター"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Japan Aerospace Exploration Agency Wind Tunnel Technology Center, Institute of Aerospace Technology"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"渡利, 實"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Watari, Minoru","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":"63330004.pdf","filesize":[{"value":"1.1 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"63330004.pdf","url":"https://jaxa.repo.nii.ac.jp/record/5839/files/63330004.pdf"},"version_id":"3a69a697-d03e-4c5c-a474-600a2665d168"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"気体モデル","subitem_subject_scheme":"Other"},{"subitem_subject":"理想気体","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"マッハ数","subitem_subject_scheme":"Other"},{"subitem_subject":"空気力","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点圧力","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速流","subitem_subject_scheme":"Other"},{"subitem_subject":"よどみ点温度","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic wind tunnel","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"air model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"ideal gas","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Mach number","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic force","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation pressure","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"stagnation 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":"JAXA極超音速風洞で用いている気体モデル","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"JAXA極超音速風洞で用いている気体モデル"}]},"item_type_id":"5","owner":"1","path":["1014","1891"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"5839","relation_version_is_last":true,"title":["JAXA極超音速風洞で用いている気体モデル"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-21T08:07:41.372082+00:00"}