@inproceedings{oai:jaxa.repo.nii.ac.jp:00003857,
 author = {南部, 太介 and 橋本, 敦 and 青山, 剛史 and 佐藤, 哲也 and Nambu, Taisuke and Hashimoto, Atsushi and Aoyama, Takashi and Sato, Tetsuya},
 book = {宇宙航空研究開発機構特別資料: 第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム論文集, JAXA Special Publication: Proceedings of the 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium},
 month = {Mar},
 note = {第46回流体力学講演会/第32回航空宇宙数値シミュレーション技術シンポジウム (2014年7月3日-4日. 弘前文化センター), 弘前市, 青森県, 46th Fluid Dynamics Conference / 32nd Aerospace Numerical Simulation Symposium (July 3-4, 2014. Hirosaki Bunka Center), Hirosaki, Aomori, Japan, The wall interference effect of the ONERA-M6 wind tunnel testing is analyzed using CFD analysis. The computational domain includes the wind tunnel walls, and the effect of the porous walls, which are set at the top and bottom of the test section, are computed by the porous wall model. The computational result gets almost the same shock wave shape as the experiment, which could not be captured in the past works. The interference by the porous walls decrease the Mach number and the incidence, and the swept angle of front shock wave and the location of rear shock wave are altered. The lift and drag coefficients are also affected by the interference of the porous wall. The lift coefficient becomes small due to decrease of the incidence. The smaller Mach number decreases drag coefficient, meanwhile decrease of the attack angle causes additional drag by similar mechanism to induced drag., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA1530023022, レポート番号: JAXA-SP-14-010},
 pages = {121--126},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {ONERA-M6風洞試験における風洞壁干渉の影響の検証},
 volume = {JAXA-SP-14-010},
 year = {2015}
}