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