{"created":"2023-06-20T15:08:23.320483+00:00","id":37824,"links":{},"metadata":{"_buckets":{"deposit":"72ecff25-a81f-47ca-9904-57719aaa1ba3"},"_deposit":{"created_by":1,"id":"37824","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37824"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037824","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["430487","430485","430486","430488"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Special Publication of National Aerospace Laboratory. Proceedings of the 12th NAL symposium on aircraft computational aerodynamics: CFD workshop on hypersonic flow"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1994-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"197","bibliographicPageStart":"1","bibliographicVolumeNumber":"26","bibliographic_titles":[{"bibliographic_title":"航空宇宙技術研究所特別資料"},{"bibliographic_title":"Special Publication of National Aerospace Laboratory","bibliographic_titleLang":"en"}]}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"H-2ロケット初号機を用いて行われた軌道再突入実験(OREX)の計測データを利用して、極超音速流に関するCFD(計算空気力学)の検証を行うためワークショップが開催され、その論文集として合計12編の報告を集めた。ワークショップ参加者は、OREX飛行体まわりの流れ、航技研極超音速風洞試験に対応する流れおよびアーク加熱風洞内の流れに関するさまざまな課題についての計算結果を提出した。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Altogether 12 participants contributed to the workshop on the hypersonic CFD (Computational Fluid Dynamics) validation using the data obtained with the OREX (Orbital Reentry Experiment) flight carried out by taking the opportunity of the initial launch test of H-2 rocket. The participants have submitted the numerical simulation results on a variety of flow cases corresponding to the real flight, the NAL hypersonic wind tunnel test and the NAL arc-heated wind tunnel test.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0004173000","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: NAL SP-26","subitem_description_type":"Other"}]},"item_5_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_5_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_5_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","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":"AN10097345","subitem_source_identifier_type":"NCID"}]},"item_5_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"航空機計算空気力学シンポジウム運営委員会"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Organizing Committee of NAL Symposium on Aircraft Computational Aerodynamics"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"航空機計算空気力学シンポジウム運営委員会"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"航空宇宙技術研究所"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Organ. Commit. of NAL Symp.","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"National Aerospace Laboratory","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":"2020-01-24"}],"displaytype":"detail","filename":"nalsp00026.pdf","filesize":[{"value":"9.5 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp00026.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37824/files/nalsp00026.pdf"},"version_id":"ee9aad53-63fe-4685-ad97-c6cb3c05f68c"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"極超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"流れ数値シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ･ストークス方程式","subitem_subject_scheme":"Other"},{"subitem_subject":"再突入実験機","subitem_subject_scheme":"Other"},{"subitem_subject":"物体の周りの流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD解析","subitem_subject_scheme":"Other"},{"subitem_subject":"非平衡流れ","subitem_subject_scheme":"Other"},{"subitem_subject":"極超音速飛行体","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"空力加熱","subitem_subject_scheme":"Other"},{"subitem_subject":"数値解析","subitem_subject_scheme":"Other"},{"subitem_subject":"軌道再突入実験","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical flow simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamic","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes equation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"reentry vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flow around body","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"OREX","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"nonequilibrium flow","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"hypersonic flight vehicle","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","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"},{"subitem_subject":"orbital reentry experiment","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":"航空宇宙技術研究所特別資料　第12回航空機計算空気力学シンポジウム論文集:特別企画/極超音速流のCFDワークショップ","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航空宇宙技術研究所特別資料　第12回航空機計算空気力学シンポジウム論文集:特別企画/極超音速流のCFDワークショップ"}]},"item_type_id":"5","owner":"1","path":["1891","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"37824","relation_version_is_last":true,"title":["航空宇宙技術研究所特別資料　第12回航空機計算空気力学シンポジウム論文集:特別企画/極超音速流のCFDワークショップ"],"weko_creator_id":"1","weko_shared_id":1},"updated":"2023-06-20T19:13:11.165157+00:00"}