@inproceedings{oai:jaxa.repo.nii.ac.jp:00004739,
 author = {荻野, 純 and 渡辺, 重哉 and 口石, 茂 and 加藤, 裕之 and 山本, 寛 and 大海, 謙一 and Ogino, Jun and Watanabe, Shigeya and Kuchiishi, Shigeru and Kato, Hiroyuki and Yamamoto, Hiroshi and Ogai, Kenichi},
 book = {宇宙航空研究開発機構特別資料: 第42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2010 論文集, JAXA Special Publication: Proceedings of 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010},
 month = {Feb},
 note = {第42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2010 (2010年6月24日-25日. 米子コンベンションセンター BiG SHiP), 42nd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2010 (June 24-25,  2010. Yonago Convention Center BiG SHiP), Yonago, Tottori Japan, In a functional part of the Digital/Analog Hybrid Wind Tunnel, planning the wind tunnel test efficiently in advance and reducing troubles about experimental apparatus placement are required. EFD Setting Simulation (ESS) system actualizes such requirements by providing a virtual environment of the transonic wind tunnel facilities and airplane scale models with three-dimensional CAD application (CATIA V5) and enables to plan several kinds of wind tunnel tests including PSP/PIV measurements instantly. The ESS system is aiming at higher usability by means of convenient user-interface with EXCEL-VBA and automated manipulation of CAD data. In the PSP simulation function of the system, for example, user can easily check their plan for PSP instrumentation setting through the virtual PSP camera views only by inputting specifications and positions about camera and lighting. The target of the present ESS system is JAXA's 2m x 2m transonic wind tunnel and will be extended to other wind tunnels. It is also planed additional functions such as CFD grid generation from the verified EFD setting information. Further system automation, enhancement of the implemented functions, additional new functions, and improvement of operability are needed in order to make the ESS system indispensable to plan the wind tunnel test., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967032, レポート番号: JAXA-SP-10-012},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {ハイブリッド風洞における風試セッティングシミュレーション},
 volume = {JAXA-SP-10-012},
 year = {2011}
}