@inproceedings{oai:jaxa.repo.nii.ac.jp:00004910,
 author = {口石, 茂 and 渡辺, 重哉 and 加藤, 裕之 and 青山, 剛史 and 村上, 桂一 and 橋本, 敦 and 藤田, 直行 and 松尾, 裕一 and 船江, 幸弘 and 荻野, 純 and Kuchiishi, Shigeru and Watanabe, Shigeya and Kato, Hiroyuki and Aoyama, Takashi and Murakami, Keiichi and Hashimoto, Atsushi and Fujita, Naoyuki and Matsuo, Yuichi and Funae, Yukihiro and Ogino, Jun},
 book = {宇宙航空研究開発機構特別資料: 第41回流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2009論文集, JAXA Special Publication: Proceedings fo 41st Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2009},
 month = {Feb},
 note = {平成21年6月18-19日. 宇宙航空研究開発機構調布航空宇宙センター, June 18-19, 2009, Japan Aerospace Exploration Agency, As a trial of the integration of Experimental Fluid Dynamics (EFD) and CFD, development of a system called Digital/Analog Hybrid Wind Tunnel is introduced. The aim of the system is to improve efficiency, accuracy, and reliability of the aerodynamic characteristics evaluation in aerospace vehicle developments through the complementary use of EFD and CFD. In the present article, key functions of the system determined as a series of preliminary design are described in detail and technical issues in the system development are addressed from the viewpoint of the EFD/CFD integration., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064672012, レポート番号: JAXA-SP-09-011},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {JAXAにおけるEFD/CFD融合に向けた試み: デジタル/アナログ・ハイブリッド風洞構想（第2報）},
 volume = {JAXA-SP-09-011},
 year = {2010}
}