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

Table 3

Results obtained through the FFSQP method (2).

Centers’ combination C(5,15)
Airfoil		UBI_03_016	DAE-21
FFSQP 3.7	Form factor	0.185	0
	REL.P	1.823%	2.22%
	GT [s]	4.63	0.375
Form factor = 0	REL.P	2.04%	2.22%
	GT [s]	0.047	0.047