Distributed micro-roughness coatings achieve up to 43.6% aerodynamic drag reduction on a streamlined model in transitional flow primarily through boundary layer friction modification.
& Obayashi, S.2024bEffects of surface roughness and free-stream turbulence on transitions in the swept-wing boundary layer
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DMR effect on drag reduction of a streamlined body measured by Magnetic Suspension and Balance System
Distributed micro-roughness coatings achieve up to 43.6% aerodynamic drag reduction on a streamlined model in transitional flow primarily through boundary layer friction modification.