{"created":"2023-06-20T15:11:39.271856+00:00","id":41347,"links":{},"metadata":{"_buckets":{"deposit":"36f1fed2-68a3-456e-aa24-b132172e33e8"},"_deposit":{"created_by":1,"id":"41347","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41347"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041347","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489605","489609","489607","489608","489606","489610","489611","489604"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Aeroelastic/structural coupled simulation of a simple aircraft configuration using the CASPER"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"260","bibliographicPageStart":"255","bibliographicVolumeNumber":"46","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_3_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 7-9 Jun. 2000 東京 日本","subitem_description_type":"Other"}]},"item_3_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 7-9 Jun. 2000 Tokyo Japan","subitem_description_type":"Other"}]},"item_3_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"CASPER(航空機性能評価システム)は、防衛庁技術本部(TRDIJDA)の主導の下に国内航空機メーカが共同開発した計算コードで、種々の最新鋭航空機の空力設計のためにCFD(計算流体力学)解析コードをベースにした設計システムである。本研究では、設計の構造計算と空力特性計算の間で対話的に繰り返し、または自動的な反復計算を行うコードであるCASPERの中の空弾性モジュールを、簡易航空機モデルを用いて評価した。また、CASPERの空力計算と有限要素法で求めた静的力学特性との連成シミュレーションの結果を、簡易航空機モデルを用いて種々の条件下で比較した。その結果、今回のオートループ計算アルゴリズムが検証した全ての場合で、良好な収束解を与えることを確証した。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"The CASPER (Computational Aerodynamics System for Performance Evaluation and Research), which has been developed under the leadership of TRDIJDA (Technical Research and Development Institute of Japan Defense Agency) with domestic aerospace makers, is a CFD (Computational Fluid Dynamics)-based design system for the aerodynamic design for various advanced aircraft. In this study, the aeroelastic module in CASPER, which is a code of iterative or automatic iteration between structural and aerodynamic computation, was evaluated by using a simple aircraft model. Also, coupled simulation results for aerodynamic computation data by CASPER and static mechanical properties obtained by the finite element method were compared under various conditions for a simple aircraft model. It was confirmed that the present auto-loop computation algorithm could give reasonable converging solutions in all the cases studied.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635046","subitem_description_type":"Other"}]},"item_3_description_33":{"attribute_name":"レポート番号","attribute_value_mlt":[{"subitem_description":"レポート番号: NAL SP-46","subitem_description_type":"Other"}]},"item_3_publisher_8":{"attribute_name":"出版者","attribute_value_mlt":[{"subitem_publisher":"航空宇宙技術研究所"}]},"item_3_publisher_9":{"attribute_name":"出版者（英）","attribute_value_mlt":[{"subitem_publisher":"National Aerospace Laboratory (NAL)"}]},"item_3_source_id_21":{"attribute_name":"ISSN","attribute_value_mlt":[{"subitem_source_identifier":"0289-260X","subitem_source_identifier_type":"ISSN"}]},"item_3_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_3_text_6":{"attribute_name":"著者所属","attribute_value_mlt":[{"subitem_text_value":"三菱重工業"},{"subitem_text_value":"防衛庁 技術研究本部　第3研究所"},{"subitem_text_value":"防衛庁 技術研究本部　第3研究所"},{"subitem_text_value":"三菱重工業"}]},"item_3_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":"Japan Defense Agency 3rd Research Center, Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Japan Defense Agency 3rd Research Center, Technical Research and Development Institute"},{"subitem_text_language":"en","subitem_text_value":"Mitsubishi Heavy Industries Ltd"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"石黒, 満津夫"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"沖, 良篤"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"酒田, 威志"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"長畑, 正史"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Ishiguro, Mitsuo","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Oki, Yoshiatsu","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Sakata, Takeshi","creatorNameLang":"en"}],"nameIdentifiers":[{}]},{"creatorNames":[{"creatorName":"Nagahata, Masashi","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":"nalsp0046046.pdf","filesize":[{"value":"1.8 MB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046046.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41347/files/nalsp0046046.pdf"},"version_id":"16a3dad2-fb85-45d7-844b-7523b10a5e37"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"CASPER","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機概念設計","subitem_subject_scheme":"Other"},{"subitem_subject":"空力-構造連成","subitem_subject_scheme":"Other"},{"subitem_subject":"空弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"空力解析","subitem_subject_scheme":"Other"},{"subitem_subject":"連成シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"飛行シミュレーション","subitem_subject_scheme":"Other"},{"subitem_subject":"収束履歴","subitem_subject_scheme":"Other"},{"subitem_subject":"構造静解析","subitem_subject_scheme":"Other"},{"subitem_subject":"荷重倍数","subitem_subject_scheme":"Other"},{"subitem_subject":"性能","subitem_subject_scheme":"Other"},{"subitem_subject":"航空機形状","subitem_subject_scheme":"Other"},{"subitem_subject":"TRDIJDA","subitem_subject_scheme":"Other"},{"subitem_subject":"CASPER","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft conceptual design","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic and structural coupling","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aerodynamic analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"coupled simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flight simulation","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"conversion history","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"structural static analysis","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"load factor","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"performance","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"aircraft configuration","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"TRDIJDA","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":"technical report","resourceuri":"http://purl.org/coar/resource_type/c_18gh"}]},"item_title":"CASPERを用いた簡易航空機形態の空力・構造連成シミュレーション","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"CASPERを用いた簡易航空機形態の空力・構造連成シミュレーション"}]},"item_type_id":"3","owner":"1","path":["1893","1915"],"pubdate":{"attribute_name":"公開日","attribute_value":"2015-03-26"},"publish_date":"2015-03-26","publish_status":"0","recid":"41347","relation_version_is_last":true,"title":["CASPERを用いた簡易航空機形態の空力・構造連成シミュレーション"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:02:36.069493+00:00"}