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- W1974762012 abstract "The flux splitting method of Van Leer (1982) and an implicit, upwind-biased, finite-volume scheme of Rumsey (1985) for solving the two-dimensional Reynolds-averaged Navier-Stokes equations were applied to analyze five airfoil geometries (the NACA 0012, 12-percent Joukowski, NACA 4412, NACA 65-015, and LS1-0417 sections), at high angles of attack. The effect of grid density and grid extent on the Strouhal number of the unsteady flow was computed, as well as the effect of variations in Mach number, Reynolds number, and angle of attack. It was found, that past an angle of attack of 20 deg, Strouhal numbers were independent of angle of attack (at a constant value of 0.115), agreeing well with the experimental findings of Tyler (1931)." @default.
- W1974762012 created "2016-06-24" @default.
- W1974762012 creator A5050028791 @default.
- W1974762012 date "1987-03-24" @default.
- W1974762012 modified "2023-09-27" @default.
- W1974762012 title "A computational analysis of flow separation over five different airfoil geometries at high angles-of-attack" @default.
- W1974762012 cites W1981202981 @default.
- W1974762012 doi "https://doi.org/10.2514/6.1987-188" @default.
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