@inproceedings{oai:jaxa.repo.nii.ac.jp:00004258,
 author = {菅原, 瑛明 and 田辺, 安忠 and 齊藤, 茂 and Sugawara, Hideaki and Tanabe, Yasutada and Saito, Shigeru},
 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, This paper describes the influence of fidelity of CFD geometry model on the accuracy of prediction compared with the JAXA Multipurpose Rotor Test System (JMRTS) experimental database. It is found that the blade grip has strong influence to the pressure distribution around the hub area, while the mast model increases the predicted accuracy on the fuselage surface downstream. It is also found that the existence of the fuselage model shows noticeable effect on the BVI strength. Although the complete complicated rotating details of the rotor hub are difficult to be included in the CFD geometry models, above simplified geometry models can deliver quite satisfactory prediction accuracy compared with experiments., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958018, レポート番号: JAXA-SP-12-010},
 pages = {109--114},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {ロータ試験データベースとの検証計算におけるモデル忠実度の影響},
 volume = {JAXA-SP-12-010},
 year = {2013}
}