Research Article

Online Projective Integral with Proper Orthogonal Decomposition for Incompressible Flows Past NACA0012 Airfoil

Figure 11

Periodic case: . Computed lift coefficient for with various number of . From top to bottom: , and 5.
264693.fig.0011a
(a)
264693.fig.0011b
(b)
264693.fig.0011c
(c)