Abstract:The effect of suction on airfoil surface at various locations downstream of the leadingedge of a thin flat-plate airfoil was studied in a wind tunnel at a low Reynolds number. At post-stall angles of attack, substantial lift enhancement and delay of stall can be achieved if a large separation bubble is generated by reattaching the massively separated flow near the trailing-edge. The effects of location and volumetric flow rate of suction were investigated by means of force and velocity measurements. There is a… Show more
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