International Journal of Aerospace Engineering / 2021 / Article / Fig 7

Research Article

A Parametric Design Method for Hybrid Airfoils for Icing Wind Tunnel Test

Figure 7

Pressure distribution for NACA0012 at (a) 0° AoA and (b) 4° AoA.

Article of the Year Award: Outstanding research contributions of 2020, as selected by our Chief Editors. Read the winning articles.