@inproceedings{oai:jaxa.repo.nii.ac.jp:00004396,
 author = {保江, かな子 and 口石, 茂 and 橋本, 敦 and 村上, 桂一 and 加藤, 裕之 and 中北, 和之 and 渡辺, 重哉 and 菱田, 学 and Yasue, Kanako and Kuchiishi, Shigeru and Hashimoto, Atsushi and Murakami, Keiichi and Kato, Hiroyuki and Nakakita, Kazuyuki and Watanabe, Shigeya and Hishida, Manabu},
 book = {宇宙航空研究開発機構特別資料: 第43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2011論文集, JAXA Special Publication: Proceedings of 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011},
 month = {Mar},
 note = {第43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2011 (2011年7月7日-8日. 早稲田大学国際会議場) 東京, 43rd Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2011 (July 7-8,  2011. Waseda University, International Conference Center), Tokyo Japan, Modification approach of a CFD surface mesh are examined using measurement data of wind tunnel model deformation, Model deformation measurements (MDM) were successfully made at JAXA using stereo photogrammetry with markers. The model's deformation was then approximated using a deformation law which is identified by a few parameters with markers attached on the wind tunnel model. This approach was developed by Le Sant to correct the model deformation effect in pressure-sensitive paint (PSP) images. In this paper, the approach is used to rearrange the CFD surface mesh of a CFD model to conform its configuration with that of the wind tunnel test model. We duplicate the deformed configuration of the wind tunnel model using three deformation laws and examine the resulting CFD models. A high-fidelity RANS simulation of the DLR-F6 Fx2B wind tunnel model is then performed considering the static deformation of the model and the effect of model deformation on the aerodynamic characteristics are also explored by performing the CFD simulation for the deformed configuration as well as the original (non-deformed) configuration., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065207024, レポート番号: JAXA-SP-11-015},
 pages = {143--148},
 publisher = {宇宙航空研究開発機構, Japan Aerospace Exploration Agency (JAXA)},
 title = {模型変形計測データを反映したCFD表面格子修正法の検討},
 volume = {JAXA-SP-11-015},
 year = {2012}
}