International Journal of Aerospace Engineering / 2013 / Article / Fig 1

Research Article

Numerical Simulation of Airfoil Aerodynamic Penalties and Mechanisms in Heavy Rain

Figure 1

(a) O-type computational domain of meshes for both the original and numerically tripped NACA 64-210 airfoils; (b) near mesh of the original airfoil; (c) near mesh of the airfoil tripped at 5% chordwise station; (d) close view of the tripped position on the 5% chordwise tripped airfoil.
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(a)
590924.fig.001b
(b)
590924.fig.001c
(c)
590924.fig.001d
(d)

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