{"created":"2023-06-20T15:07:58.113993+00:00","id":37346,"links":{},"metadata":{"_buckets":{"deposit":"12327f04-da90-4c7f-840f-e4c2ac80b272"},"_deposit":{"created_by":1,"id":"37346","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37346"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037346","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480261","480260"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Numerical analysis on HSCT model, part 3"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"220","bibliographicPageStart":"215","bibliographicVolumeNumber":"41","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_14":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）","attribute_value_mlt":[{"subitem_description":"航空宇宙技術研究所 24-26 Jun. 1998 東京 日本","subitem_description_type":"Other"}]},"item_5_description_15":{"attribute_name":"会議概要（会議名, 開催地, 会期, 主催者等）（英）","attribute_value_mlt":[{"subitem_description":"National Aerospace Laboratory 24-26 Jun. 1998 Tokyo Japan","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"HSCT(高速民間輸送機)模型周りの数値流れ場解析をマルチグリッド・オイラーコードを用いて実行した。結果は、NALによって行われた超音速風洞試験の結果と比較することによって評価した。圧力積分値(CLおよびCM)においては、数値結果は風洞試験結果とよく一致した。抵抗係数に関しては、オイラーコードの結果に境界層補正を行った。この補正により、迎角による抗力(CD)はオイラーコードによる計算結果よりも風洞試験結果により近くなった。これら全ての解析は、EWSを用いて1ケース当たり4時間を要した。予備的な空力試験の段階においては、合理的な時間および品質水準であると思われる。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Numerical flow analysis around the HSCT (High Speed Civil Transport) model was carried out using multi grid Euler code. The results are evaluated by comparing with results of supersonic wind tunnel test that was conducted by NAL. The numerical results were well agreed with wind tunnel test results in pressure integrated value (CL, CM). As for the drag coefficient, the boundary layer correction was performed to results of Euler code and it made the drag (CD) closer to wind tunnel results than original Euler results. All these analysis took four hours/case on EWS and it seems reasonable time and quality level for preliminary aerodynamics examination phase.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958032","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-41","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":"富士重工業"}]},"item_5_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"Fuji Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"若井, 洋"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Wakai, Hiroshi","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":"2020-02-10"}],"displaytype":"detail","filename":"nalsp0041032.pdf","filesize":[{"value":"544.5 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0041032.pdf","url":"https://jaxa.repo.nii.ac.jp/record/37346/files/nalsp0041032.pdf"},"version_id":"751289dd-6c24-4941-ac81-d5b534eabe8e"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"HSCT模型","subitem_subject_scheme":"Other"},{"subitem_subject":"高速民間輸送機模型","subitem_subject_scheme":"Other"},{"subitem_subject":"マルチグリッド・オイラーコード","subitem_subject_scheme":"Other"},{"subitem_subject":"超音速風洞試験","subitem_subject_scheme":"Other"},{"subitem_subject":"圧力積分値","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"数値流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"抵抗係数","subitem_subject_scheme":"Other"},{"subitem_subject":"境界層補正","subitem_subject_scheme":"Other"},{"subitem_subject":"HSCT model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"high speed civil transport model","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"multi grid Euler code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"supersonic wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"pressure integrated value","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"drag coefficient","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"boundary layer correction","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":"HSCT模型の数値解析　その3","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HSCT模型の数値解析　その3"}]},"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":"37346","relation_version_is_last":true,"title":["HSCT模型の数値解析　その3"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:21:20.780702+00:00"}