Airfoil-Wake Modification with Gurney Flap at Low Reynolds Number
نویسندگان
چکیده
منابع مشابه
Plunging Airfoil Load Characteristics Equipped with Gurney Flap
Numerous experiments have been conducted on plunging Eppler 361 airfoil in a subsonic wind tunnel. The experimental tests involved measuring the surface pressure distribution over the airfoil at Re=1.5×105. The airfoil was equipped with Gurney flap(heights of 2.6, 3.3 and 5% chord) and plunged at 6cm amplitude. The unsteady aerodynamic loads were calculated from the surface pressure measurement...
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ژورنال
عنوان ژورنال: AIAA Journal
سال: 2018
ISSN: 0001-1452,1533-385X
DOI: 10.2514/1.j056260