Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation

<table>Comparison of an analytical NACA 0012 airfoil (upper surface only) with one obtained by using the Bezier curves of orders 7 and 11. The plots represent an excellent agreement between the analytical NACA and the Bezier of order 11.</table>

Mathematical Problems in Engineering

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Figure 31

Figure 31: Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation 