Use of Multiquadric Functions for Multivariable Representation of the Aerodynamic Coefficients of Airfoils

Table 4

Results obtained through the FFSQP method (3).

Centers’ combination C(5,30)
Airfoil		UBI_03_016	DAE-21
FFSQP 3.7	Form factor	0	0.007
	REL.P	0.73%	1.28%
	GT [s]	4.86	23.19
Form factor = 0	REL.P	0.73%	2.03%
	GT [s]	0.094	0.094