{"created":"2023-06-20T14:37:24.929587+00:00","id":3824,"links":{},"metadata":{"_buckets":{"deposit":"c8cd9a7b-36d9-483e-a959-537b596b109c"},"_deposit":{"created_by":1,"id":"3824","owners":[1],"pid":{"revision_id":0,"type":"depid","value":"3824"},"status":"published"},"_oai":{"id":"oai:jaxa.repo.nii.ac.jp:00003824","sets":["1887:1891","9:789:855:858"]},"author_link":["16039","16037","16042","16038","16045","16036","16034","16041","16043","16050","16047","16051","16044","16035","16049","16046","16048","16040"],"item_5_alternative_title_2":{"attribute_name":"その他のタイトル（英）","attribute_value_mlt":[{"subitem_alternative_title":"Current Status of the Development of JAXA Digital/Analog-Hybrid Wind 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2012)","subitem_description_type":"Other"}]},"item_5_description_16":{"attribute_name":"抄録","attribute_value_mlt":[{"subitem_description":"宇宙航空研究開発機構（JAXA）では、現状の風洞（実流れを対象とした「アナログ風洞」）に対してCFD（数値シミュレーションという意味での「デジタル風洞」）を強く連携させたコンカレントなEFD/CFD 融合システムである、「デジタル/アナログ・ハイブリッド風洞」の開発を現在進めている。ハイブリッド風洞ではEFD（風洞）/CFD 両者に固有な弱点・技術課題を相補的に解決するとともに、EFD/CFD 両データを統一的に生産・管理して対等な比較検証が可能なプラットフォームを整備することにより、EFD/CFD 両者の有用性を向上させ、航空・宇宙機の設計時間/コスト/リスクの低減、設計データ精度/信頼性の改善を行うことを目指す。現在の開発ステータスとしては、試行システムをJAXA 2m×2m 遷音速風洞における実風洞試験に適用して課題・問題点を抽出すると共に、EFD/CFD 両者の融合をより高めた機能の研究開発を進めているところである。本稿では、平成23 年度以降、新たに追加となった機能について概要を紹介すると共に、風試適用結果（DLR-F6 形状模型PSP/PIV/模型変形同時計測試験）を示す。","subitem_description_type":"Abstract"}]},"item_5_description_18":{"attribute_name":"内容記述","attribute_value_mlt":[{"subitem_description":"形態: カラー図版あり","subitem_description_type":"Other"}]},"item_5_description_19":{"attribute_name":"内容記述（英）","attribute_value_mlt":[{"subitem_description":"Physical characteristics: Original contains color 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