Research Article
Aerodynamic Optimal Shape Design Based on Body-Fitted Grid Generation
Table 13
Comparison of the pressure at the maximum thicknesses of the airfoil surface (upper and lower surfaces) for the initial, optimal, and desired shapes.
| ā | Initial shape | Optimal shape | Desired shape | Difference (Pa) |
| Pressure at (Pa) | | | | Difference in initial and desired = 2150.84 Difference in optimal and desired = 0.60 | Pressure at (Pa) | | | | Difference in initial and desired = 1833.24 Difference in optimal and desired = 0.89 |
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