Computational study of flow around a NACA 0012 by using Roe FVM scheme and davis-yee TVD scheme
Sign Up to like & getrecommendations! Published in 2019 at "Indonesian Journal of Electrical Engineering and Computer Science"
DOI: 10.11591/ijeecs.v16.i2.pp1018-1025
Abstract: Currently CFD had been considered as an important tool for solving engineering problems. The application of CFD had been used intensively in aircraft industries in design a new aircraft or in the effort of improvement… read more here.
Keywords: naca 0012; scheme; computer code; computer ... See more keywords
Numerical investigation of the effect of triangular cavity on the unsteady aerodynamics of NACA 0012 at a low Reynolds number
Sign Up to like & getrecommendations! Published in 2021 at "Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering"
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
Self-noise of NACA 0012 and NACA 0021 aerofoils at the onset of stall
Sign Up to like & getrecommendations! Published in 2017 at "International Journal of Aeroacoustics"
DOI: 10.1177/1475472x17709929
Abstract: The aerodynamic noise of a NACA 0012 and NACA 0021 aerofoil is measured and compared in order to determine whether there are differences in their noise signatures with a focus on the onset of stall.… read more here.
Keywords: naca 0021; noise naca; self noise; 0012 naca ... See more keywords
Unsteady aerodynamics of a pitching NACA 0012 airfoil at low Reynolds number
Sign Up to like & getrecommendations! Published in 2019 at "International Journal of Micro Air Vehicles"
DOI: 10.1177/1756829319890609
Abstract: The present paper aims to investigate numerically small amplitude oscillation of NACA 0012 airfoil at Re = 1000. The airfoil is sinusoidally pitching around the quarter chord point with 1° pitch amplitude about a mean angle of… read more here.
Keywords: aerodynamics pitching; unsteady aerodynamics; 0012 airfoil; aerodynamics ... See more keywords