@inproceedings{oai:jaxa.repo.nii.ac.jp:00004268,
 author = {南部, 太介 and 橋本, 敦 and 砂田, 茂 and 佐藤, 哲也 and Nambu, Taisuke and Hashimoto, Atsushi and Sunada, Shigeru and Sato, Tetsuya},
 book = {宇宙航空研究開発機構特別資料, JAXA Special Publication: Proceedings of 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012},
 month = {Mar},
 note = {第44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2012 (2012年7月5日-6日. 富山国際会議場大手町フォーラム), 富山市, 富山県, 44th Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2012 (July 5-6, 2012. Toyama International Conference Center), Toyama Japan, To make an actuator disc model, a propeller for low Reynolds number flow is computed by the moving mesh method. We compare results by different CFD methods in terms of the turbulence model and time integration method. In the design condition, the results computed by the unsteady time integration method without the turbulence model agree well with the results computed by Adkins-Liebeck method. An actuator disc model is created using the force distribution computed by CFD. Velocity distribution of wake computed by the model partially agrees with one computing propeller's geometry directly. However, some errors are caused by the defects of modeling blade tip vortex and turbulent viscosity., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958028, レポート番号: JAXA-SP-12-010},
 pages = {167--172},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {移動格子法による低Re数用Propeller流れの数値解析},
 volume = {JAXA-SP-12-010},
 year = {2013}
}