@inproceedings{oai:jaxa.repo.nii.ac.jp:00004261,
 author = {南部, 太介 and 佐藤, 哲也 and 橋本, 敦 and 上野, 真 and 村上, 桂一 and Nambu, Taisuke and Sato, Tetsuya and Hashimoto, Atsushi and Ueno, Makoto and Murakami, Keiichi},
 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, The Mokry’s correction method for the wind tunnel wall interference is verified by CFD analysis with porous wall model. The wall interference correction is applied to the CFD result of the flow around NACA0012 airfoil with wind tunnel walls, and then this corrected result is compared with the one without wind tunnel walls. The Mokry’s method shows high accuracy under subsonic and low incident angle condition even if blockage ratio is so large. However, about 10 drag count error is caused under the transonic flow. Flow separation　decreases the accuracy significantly and it shows the Mokry’s method is not appropriate for stall condition., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0061958021, レポート番号: JAXA-SP-12-010},
 pages = {127--132},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {多孔壁モデルを用いたＣＦＤ解析による風洞壁干渉補正法の検証},
 volume = {JAXA-SP-12-010},
 year = {2013}
}