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Development of Digital Wind Tunnel as a Subsystem of JAXA Digital/Analog Hybrid Wind Tunnel
https://jaxa.repo.nii.ac.jp/records/4111
https://jaxa.repo.nii.ac.jp/records/4111ac4c4fea-19ea-410d-a3c3-7ed549800d71
名前 / ファイル | ライセンス | アクション |
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62070003.pdf (294.2 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Development of Digital Wind Tunnel as a Subsystem of JAXA Digital/Analog Hybrid Wind Tunnel | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | digital wind tunnel | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | computational fluid dynamics | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
著者 |
村上, 桂一
× 村上, 桂一× 橋本, 敦× 菱田, 学× Lahur, Paulus R.× 国枝, 明× 渡辺, 重哉× Murakami, Keiichi× Hashimoto, Atsushi× Hishida, Manabu× Lahur, Paulus R.× Kunieda, Akira× Watanabe, Shigeya |
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著者所属 | ||||||
宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部数値解析グループ(JAXA) | ||||||
著者所属 | ||||||
株式会社菱友システムズ エンジニアリングソリューション事業部 | ||||||
著者所属 | ||||||
株式会社計算力学研究センター | ||||||
著者所属 | ||||||
株式会社シーイーシー(CEC) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発本部風洞技術開発センター(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Numerical Analysis Group, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Engineering Solution Division, Ryoyu Systems Co., Ltd. | ||||||
著者所属(英) | ||||||
en | ||||||
Research Center of Computational Mechanics, Inc. | ||||||
著者所属(英) | ||||||
en | ||||||
Computer Engineering & Consulting, Ltd. (CEC) | ||||||
著者所属(英) | ||||||
en | ||||||
Wind Tunnel Technology Center, Aerospace Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構(JAXA) | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication 巻 JAXA-SP-13-001E, p. 29-35, 発行日 2013-11-30 |
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会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Japan Aerospace Exploration Agency (JAXA) is developing a practical Experimental Fluid Dynamics and Computational Fluid Dynamics (EFD/CFD) integration system called the Digital/Analog Hybrid Wind Tunnel(DAHWIN), where ‘Digital’ and ‘Analog’ denote CFD and EFD (or wind tunnel), respectively. The aim of thissystem is to improve effectiveness, accuracy, and reliability of wind tunnel tests by jointly utilizing CFD as well as some advanced techniques for the EFD/CFD integration. For the development of the Digital Wind Tunnel(DWT), both features of high-speed performance and high degree of accuracy must be accomplishedsimultaneously for realizing the timely use of the DAHWIN system and high-fidelity wind tunnel data corrections. In this paper, several functions of the DWT and a newly-developed fast CFD routine for the DWTare introduced. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0062070003 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-13-001E |