AIAA Journal · 1991 · 104 citations · 4 references
EngineeringAerospace EngineeringPhysicsAerodynamicsFluid DynamicsAerodynamic DesignAirfoil TheoryExternal AerodynamicsTurbulenceTurbulent FlowWing AerodynamicsAirfoil AerodynamicsAirfoil LiftDragFlow Around AirfoilsFlow Over AirfoilsFree-stream Turbulence EffectsReynolds NumberReynolds Number Effects
The lift and drag characteristics and associated flowfields over the suction surface of an NACA 0015 airfoil with an aspect ratio of 2.9 were obtained at a Reynolds number of 250,000 for conditions both with and without freestream turbulence (FST).
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