@inproceedings{oai:jaxa.repo.nii.ac.jp:00004738,
 author = {保江, かな子 and 澤田, 恵介 and Yasue, Kanako and Sawada, Keisuke},
 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, A static aeroelasticity analysis is carried out for ONERA-M5 wind tunnel calibration model. RANS solution obtained by the pointwise relaxation implicit discontinuous Galerkin CFD solver is fed into structural analysis using NX Nastran to iteratively determine aerodynamic equilibrium configuration of the wind tunnel model. The effect of model deformation and the Reynolds number scaling effect on aerodynamic characteristics are examined. A possible CFD-aided evaluation method for obtaining the Reynolds number scaling effect using the Trisonic Wind Tunnel is discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0064967031, 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 = {Discontinuous Galerkin 法による主翼変形を考慮したONERA-M5 標準模型周りの流れ場解析},
 volume = {JAXA-SP-10-012},
 year = {2011}
}