Propagation of Shock on NREL Phase VI Wind Turbine Airfoil under Compressible Flow

Figure 9

(a) Coefficient of pressure (𝐶_𝑝) along airfoil at 𝛼=0^∘, (b) coefficient of pressure (𝐶_𝑝) along airfoil at 𝛼=2^∘, (c) coefficient of pressure (𝐶_𝑝) along airfoil at 𝛼=4^∘, and (d) coefficient of pressure (𝐶_𝑝) along airfoil at 𝛼=10^∘.

(a)

(b)

(c)

(d)