@inproceedings{oai:jaxa.repo.nii.ac.jp:00004111,
 author = {村上, 桂一 and 橋本, 敦 and 菱田, 学 and Lahur, Paulus R. and 国枝, 明 and 渡辺, 重哉 and Murakami, Keiichi and Hashimoto, Atsushi and Hishida, Manabu and Lahur, Paulus R. and Kunieda, Akira and Watanabe, Shigeya},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication},
 month = {Nov},
 note = {5th Symposium on Integrating CFD and Experiments in Aerodynamics (October 3-5, 2012, Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)), Chofu, Tokyo, Japan, 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0062070003, レポート番号: JAXA-SP-13-001E},
 pages = {29--35},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Development of Digital Wind Tunnel as a Subsystem of JAXA Digital/Analog Hybrid Wind Tunnel},
 volume = {JAXA-SP-13-001E},
 year = {2013}
}