Abstract:Distributed roughness occurs on aerodynamic surfaces like wind/gas turbine blades and aircraft wings causing early boundary layer transition resulting in higher skin friction, reduced lift-to-drag ratio, and lower power production. Despite being a recurring theme in practical engineering scenarios, the mechanism of boundary layer transition caused by distributed roughness is not well understood, and consequently, from a fluid dynamics perspective, methods for mitigating its effects are scarce. In this work, we… Show more
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