High angle-of-attack aerodynamics of a straight wing with finite span using a discrete vortex method
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DOI: 10.1063/5.0025327
Abstract: The leading-edge-suction-parameter modulated discrete vortex method is extended to a wing with a finite span and no sweep, in order to get the development of aerodynamic coefficients with an angle-of-attack, from attached to completely detached… read more here.
Keywords: vortex method; discrete vortex; angle attack; wing finite ... See more keywords