Experimental and computational investigations of aerodynamic characteristics of a finite rectangular wing-in-ground effect
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DOI: 10.1177/09544100221114700
Abstract: Wind tunnel experiments are carried out on a 3D wing-in-ground effect at pre- and post-stall angles of attack at a relatively low Reynolds number, Re ≈ 8.8 × 104. The rectangular wing, aspect ratio, AR… read more here.
Keywords: wing ground; ground; effect; ground proximity ... See more keywords