Effects of the Actuation on the Boundary Layer of an Airfoil at Reynolds Number Re = 60000
I. Rodríguez, O. Lehmkuhl, R. Borrell
Topics & Concepts
AirfoilReynolds numberAngle of attackLift coefficientAerodynamic centerFlow separationMechanicsRelative windBoundary layerChord (peer-to-peer)PhysicsLift (data mining)DragLeading edgeAerodynamicsLift-to-drag ratioLaminar flowComputer scienceTurbulenceDistributed computingData miningFluid Dynamics and Turbulent FlowsPlasma and Flow Control in AerodynamicsAerodynamics and Acoustics in Jet Flows