{"created":"2023-06-20T15:07:56.751970+00:00","id":37318,"links":{},"metadata":{"_buckets":{"deposit":"07b3a30f-83e8-4b4f-b8f0-79582ed9d774"},"_deposit":{"created_by":1,"id":"37318","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"37318"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00037318","sets":["1887:1891","1896:1898:1913:1915"]},"author_link":["480099","480102","480103","480096","480097","480098","480100","480101"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Static aeroelastic analysis for HOPE"}]},"item_5_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"1999-02","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"34","bibliographicPageStart":"29","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":"CFD(計算流体力学)解析コード(ナビエ・ストークスソルバ)と構造解析コードNASTRAN(NASA Structural Analysis computer program)を結合した静的空力弾性解析を行った。本解析法は両コードの反復法である。解析はHOPE(H-2ロケット打ち上げ型有翼回収機)について検証を行った。計算結果は弾性モデルの風洞実験結果と比較し、この解析コードの妥当性を確認するために行った。CFD解析コードは概ねこれまで用いられていた線形コードよりも良い結果が得られた。","subitem_description_type":"Abstract"}]},"item_5_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Static aeroelastic analysis that was combined with CFD (Computational Fluid Dynamics) analysis code (Navier-Stokes solver) and structural analysis code NASTRAN (NASA Structural Analysis computer program) was performed. The method is an iterative procedure of both codes. This analysis was carried out for HOPE (H-2 Orbiting Plane) configuration. The computational results were compared with those of wind tunnel tests with the elastic model in order to validate this analysis code. It concludes that CFD analysis code generally gives better results than the linear code that was used so far.","subitem_description_type":"Other"}]},"item_5_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0001958004","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":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"三菱重工業"},{"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":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"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":"本多, 淑恵"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"海田, 武司"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長畑, 正史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"中道, 二郎"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Honda, Yoshie","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Kaiden, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagahata, Masashi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nakamichi, Jiro","creatorNameLang":"en"}],"nameIdentifiers":[{}]}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CFD","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ・ストークスソルバ","subitem_subject_scheme":"Other"},{"subitem_subject":"構造解析コード","subitem_subject_scheme":"Other"},{"subitem_subject":"静的空力弾性解析","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_scheme":"Other"},{"subitem_subject":"風洞実験","subitem_subject_scheme":"Other"},{"subitem_subject":"計算流体力学","subitem_subject_scheme":"Other"},{"subitem_subject":"宇宙往還技術試験機","subitem_subject_scheme":"Other"},{"subitem_subject":"NASTRAN","subitem_subject_scheme":"Other"},{"subitem_subject":"NASA構造解析コード","subitem_subject_scheme":"Other"},{"subitem_subject":"CFD","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes solver","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural analysis code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"static aeroelastic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"HOPE","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"wind tunnel test","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"computational fluid dynamics","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"H 2 Orbiting Plane Experimental","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NASTRAN","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NASA structural analysis computer program","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":"HOPEにおける静的空力弾性解析","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"HOPEにおける静的空力弾性解析"}]},"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":"37318","relation_version_is_last":true,"title":["HOPEにおける静的空力弾性解析"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:21:57.830013+00:00"}