A new scalable Monotonically-Integrated Large Eddy Simulation (MILES) methid based on Compact Accurately Boundary-Adjasting highREsolution Technique (CABARET) has been applied for the simulation of unsteady flow around NACA0012 airfoil ar Re=408000 and M=0.115. Detailed aerodynamic analysis results are presented. For computations, two grid resolutions are considered, circa 8 and 16 million grid cells. The flow solutions is coupled with the Ffowcs Williams-Hawkings formulation for far-field noise prediction. Comparison with the experimental data is presented.