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Numerical study of separation on the trailing edge of a symmetrical airfoil at a low Reynolds number

Autor: Can Huang, Feng Guo, Juanmian Lei

Publikováno v: Chinese Journal of Aeronautics. 26:918-925

This study focuses on the trailing-edge separation of a symmetrical airfoil at a low Reynolds number. Finite volume method is adopted to solve the unsteady Reynolds-averaged Navier–Stokes (RANS) equation. Flow of the symmetrical airfoil SD8020 at a

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::3828688d3aaf233089c661621a7dac2d
https://doi.org/10.1016/j.cja.2013.06.005

Wind-tunnel pressure measurements on model-scale rigid downwind sails

Autor: Ignazio Maria Viola, Patrick Bot, Jean-Sebastien Brett, Richard G.J. Flay

Publikováno v: Ocean Engineering
Ocean Engineering, Elsevier, 2014, 90, pp.84-92. ⟨10.1016/j.oceaneng.2014.07.024⟩
The Third International Conference on Innovation in High Performance Sailing Yachts, Lorient, France
The Third International Conference on Innovation in High Performance Sailing Yachts, INNOVSAIL, Lorient, France
The Third International Conference on Innovation in High Performance Sailing Yachts, INNOVSAIL, Lorient, France, Jun 2013, Lorient, France. pp.119-127
Bot, P, Viola, I M, Flay, R G J & Brett, J-S 2014, ' Wind-tunnel pressure measurements on model-scale rigid downwind sails ', Ocean Engineering, vol. 90, pp. 84 . https://doi.org/10.1016/j.oceaneng.2014.07.024

Pressures with high spatial resolution (175 taps) on rigid model downwind sail * Leading edge separation bubble and sail curvature suction peaks clearly determined * High suction peak and sharp pressure recovery at leading edge separation bubble * Sm

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::dd80cb08e85e3cb556b4991cf72a62af
https://hal.archives-ouvertes.fr/hal-01071046/file/IRENAV_OE_2014_BOT1.pdf

Compendium CFD Workshop on 2D Airfoil Stall Prediction: Can CFD predict airfoil stall angle?

Autor: Hirose, Naoki, Nakahashi, Kazuhiro, Yoshida, Kenji, Matsuo, Yuichi, Iwamiya, Toshiyuki

Publikováno v: 航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 46:175-177

航空宇宙技術研究所 7-9 Jun. 2000 東京 日本
National Aerospace Laboratory 7-9 Jun. 2000 Tokyo Japan
「CFD(計算流体力学)は翼型失速角を予測できるか?」と題する2次元翼型失速予測に関するCFDワー�

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::3e1529c4f65ce0844b6e3ac2b8141631
http://id.nii.ac.jp/1696/00041327/

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