Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coandă Jet
Figure 2
Typical values in the turbulent boundary layer and velocity profiles in wall units for subsonic flow over flat plate, , , medium grid; nozzle pressure ratio = 1.4. (Source: Menter [23], Salim and Cheah [45], and Economon and Milholen II [46]).