Large-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6×106

No AccessTechnical NoteLarge-Eddy Simulation of NACA 0015 Airfoil Flow at Reynolds Number of 1.6×106Makoto Sato, Kengo Asada, Taku Nonomura, Soshi Kawai and Kozo FujiiMakoto SatoJapan Aerospace Exploration Agency, Sagamihara 252-5210, Japan, Kengo AsadaUniversity of Tokyo, Sagamihara 252-5210, Japan, Taku NonomuraJapan Aerospace Exploration Agency, Sagamihara 252-5210, Japan, Soshi KawaiTohoku University, Sendai 980-8579, Japan and Kozo FujiiJapan Aerospace Exploration Agency, Sagamihara 252-5210, JapanPublished Online:9 Oct 2016https://doi.org/10.2514/1.J054963SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Fureby C., "Towards the Use of Large Eddy Simulation in Engineering," Progress in Aerospace Sciences, Vol. 44, No. 6, 2008, pp. 381–396. doi:https://doi.org/10.1016/j.paerosci.2008.07.003 PAESD6 0376-0421 CrossrefGoogle Scholar[2] Fröhlich J. and von Terzi D., "Hybrid LES/RANS Methods for the Simulation of Turbulent Flows," Progress in Aerospace Sciences, Vol. 44, No. 5, 2008, pp. 349–377. doi:https://doi.org/10.1016/j.paerosci.2008.05.001 PAESD6 0376-0421 CrossrefGoogle Scholar[3] Mary I. and Sagaut P., "Large Eddy Simulation of Flow Around an Airfoil Near Stall," AIAA Journal, Vol. 40, No. 6, 2002, pp. 1139–1145. doi:https://doi.org/10.2514/2.1763 AIAJAH 0001-1452 LinkGoogle Scholar[4] Mellen C. 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