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1. 1. Active flow control of the turbulent boundary layer over a NACA4412 wing profile for skin friction drag reduction

   University essay from KTH/Teknisk mekanik

   Author : Giacomo Semprini Cesari; [2023]
   Keywords : Active flow control; drag reduction; numerical simulations; turbulent boundary layer; wings;

   Abstract : In the context of building a framework for active flow control of turbulent boundary layers in wings, a set of large-eddy simulation (LES) are implemented in OpenFOAM. The flow around a NACA4412 wing profile is simulated at 5° angle of attack and Re_c = 400˙000. READ MORE