Numerical investigation of the effect of triangular cavity on the unsteady aerodynamics of NACA 0012 at a low Reynolds number
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DOI: 10.1177/09544100211027042
Abstract: Time accurate numerical simulations were conducted to investigate the effect of triangular cavities on the unsteady aerodynamic characteristics of NACA 0012 airfoil at a Reynolds number of 50,000. Right-angled triangular cavities are placed at 10%,… read more here.
Keywords: reynolds number; cavity; aerodynamics; naca 0012 ... See more keywords