Research Article
Use of Multiquadric Functions for Multivariable Representation of the Aerodynamic Coefficients of Airfoils
Table 2
Results obtained through the FFSQP method (1).
| Centers’ combination C(5,5) |
| Airfoil | | UBI_03_016 | DAE-21 |
| FFSQP 3.7 | Form factor | 1.45 | 0.28 | REL.P | 4.40% | 6.36% | GT [s] | 4.125 | 1.09 |
| Form factor = 0 | REL.P | 16.51% | 8.91% | GT [s] | 0.0156 | 0.0156 |
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