{"created":"2023-06-20T15:11:39.545879+00:00","id":41353,"links":{},"metadata":{"_buckets":{"deposit":"47e9fd01-a622-4fbc-b401-a8f04b4349b0"},"_deposit":{"created_by":1,"id":"41353","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"41353"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00041353","sets":["1887:1893","1896:1898:1913:1915"]},"author_link":["489646","489647","489644","489645"],"item_3_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Integration of analysis program of aeroelasticity of NAL"}]},"item_3_biblio_info_10":{"attribute_name":"書誌情報","attribute_value_mlt":[{"bibliographicIssueDates":{"bibliographicIssueDate":"2000-12","bibliographicIssueDateType":"Issued"},"bibliographicPageEnd":"294","bibliographicPageStart":"291","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":"航空宇宙技術研究所(NAL)では、3次元空力弾性解析プログラムとして、線型コードDPM(ダブレットポイント法)、完全ポテンシャルコードUSTF3、オイラーコード(EL)、ナビエ-ストークス・コード(NSコード)がそれぞれ単独に開発された。この論文では、新しく構築した数値空力弾性評価試験評価系(NATAS)について述べ、関係する解析プログラムにつぃて概説した。NATASは別々に開発されたこれらのコードを統一し、全てのコードに共通する新しい計算環境を作った。これまでは有効利用と運転性能を向上することを目的にして作業した。機能の重複する別々のプログラムとコードを整理せずにそのままにして、一緒にまとめるというコンセプトのもとにプログラムの統一作業を行った。次の段階で、入力パラメータや出力データシステムの共通フォーマットを開発する。","subitem_description_type":"Abstract"}]},"item_3_description_17":{"attribute_name":"抄録（英）","attribute_value_mlt":[{"subitem_description":"Three dimensional aeroelastic analysis programs, which include linear code DPM (Doublet-Point Method), USTF3 full potential code, and EL (Euler) and NS (Navier-Stokes) codes, have individually been developed at NAL. This paper describes a newly constructed Numerical Aeroelasticity Testing and Assessment System (NATAS) and outlines involved analytical programs. The NASTAS integrates these separately developed codes into a single network system and creates a new computational environment common to all the codes. This particular activity is focused on the objective that the effective utilization and operational performance should be enhanced. Integration has been built so far on the concept that just the separate programs and codes have been put together leaving the functional duplication intact, so that some common formats on input parameters and output data systems must be developed in the next stage.","subitem_description_type":"Other"}]},"item_3_description_32":{"attribute_name":"資料番号","attribute_value_mlt":[{"subitem_description":"資料番号: AA0028635052","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":"航空宇宙技術研究所"},{"subitem_text_value":"航空宇宙技術研究所"}]},"item_3_text_7":{"attribute_name":"著者所属（英）","attribute_value_mlt":[{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"},{"subitem_text_language":"en","subitem_text_value":"National Aerospace Laboratory"}]},"item_creator":{"attribute_name":"著者","attribute_type":"creator","attribute_value_mlt":[{"creatorNames":[{"creatorName":"齊藤, 健一"}],"nameIdentifiers":[{"nameIdentifier":"489644","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"神田, 淳"}],"nameIdentifiers":[{"nameIdentifier":"489645","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Saito, Kenichi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"489646","nameIdentifierScheme":"WEKO"}]},{"creatorNames":[{"creatorName":"Kanda, Atsushi","creatorNameLang":"en"}],"nameIdentifiers":[{"nameIdentifier":"489647","nameIdentifierScheme":"WEKO"}]}]},"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":"nalsp0046052.pdf","filesize":[{"value":"352.6 kB"}],"format":"application/pdf","licensetype":"license_note","mimetype":"application/pdf","url":{"label":"nalsp0046052.pdf","url":"https://jaxa.repo.nii.ac.jp/record/41353/files/nalsp0046052.pdf"},"version_id":"c5cc7f0b-431b-498e-8acd-34ba875076be"}]},"item_keyword":{"attribute_name":"キーワード","attribute_value_mlt":[{"subitem_subject":"空力弾性","subitem_subject_scheme":"Other"},{"subitem_subject":"解析的プログラム","subitem_subject_scheme":"Other"},{"subitem_subject":"ダブレットポイント法","subitem_subject_scheme":"Other"},{"subitem_subject":"完全ポテンシャル","subitem_subject_scheme":"Other"},{"subitem_subject":"オイラーコード","subitem_subject_scheme":"Other"},{"subitem_subject":"ナビエ-ストークス・コード","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_scheme":"Other"},{"subitem_subject":"NATAS","subitem_subject_scheme":"Other"},{"subitem_subject":"数値フラッタ試験評価システム","subitem_subject_scheme":"Other"},{"subitem_subject":"フラッタ","subitem_subject_scheme":"Other"},{"subitem_subject":"線型コード","subitem_subject_scheme":"Other"},{"subitem_subject":"数値風洞","subitem_subject_scheme":"Other"},{"subitem_subject":"aeroelasticity","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"analytical program","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"doublet point method","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"full potential","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Euler code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"Navier Stokes code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NWT","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"NATAS","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical aeroelasticity testing and assessment system","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"flutter","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"linear code","subitem_subject_language":"en","subitem_subject_scheme":"Other"},{"subitem_subject":"numerical wind tunnel","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":"航技研の航空機設計プログラムの統合","item_titles":{"attribute_name":"タイトル","attribute_value_mlt":[{"subitem_title":"航技研の航空機設計プログラムの統合"}]},"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":"41353","relation_version_is_last":true,"title":["航技研の航空機設計プログラムの統合"],"weko_creator_id":"1","weko_shared_id":-1},"updated":"2023-06-20T21:02:26.395998+00:00"}