Advances in Aerodynamics

Table 1 Design variables \(c_i\) (\(\times 10^{-2}\)) [34] of the OFJ6421 airfoil in optimization. From 1 to 7 is from the leading edge to the trailing edge

From: Experimental design for a novel co-flow jet airfoil

Baseline	\(c_1\)	\(c_2\)	\(c_3\)	\(c_4\)	\(c_5\)	\(c_6\)	\(c_7\)
Upper	0.0583154	0.170103	0.6839475	1.3492515	0.7583871	0.265861	–0.0171801
Lower	–0.7997711	−0.4648966	0.4963607	0.4949874	0.0188144	0.262501	–0.8695659

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