Comparison of Numerical and Experimental Results over a NACA0025 Airfoil Undergoing Separation
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چکیده
Lin & Pauley [2] studied unsteady boundary-layer separation from an Eppler 387 airfoil at low Reynolds number numerically and compared their results with wind tunnel measurements. They found unsteady large-scale structure might control the lowReynolds-number separation bubble reattachment with smallscale turbulence playing a secondary role [4]. Drela [5], Drela & Giles[6] used a fully coupled nonlinear system and predicted transitioning separation bubbles and their associated losses.
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Comparison of Numerical and Experimental Results over a NACA0025 Airfoil Undergoing Separation
Lin & Pauley [2] studied unsteady boundary-layer separation from an Eppler 387 airfoil at low Reynolds number numerically and compared their results with wind tunnel measurements. They found unsteady large-scale structure might control the lowReynolds-number separation bubble reattachment with smallscale turbulence playing a secondary role [4]. Drela [5], Drela & Giles[6] used a fully coupled n...
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