Table 7. Component parasite drag using OpenVSP

	Wetted area (ft2)	Drag coefficient	Drag force (%)
Fuselage	373.87	0.01380	33.56
Main wing	139.83	0.00736	15.15
Vertical tail	10.09	0.00060	1.07
Duct	38.20	0.016745	28.44
Propeller	22.57	0.00914	13.99
Horizontal stabilizer	44.51	0.01439	7.25
Pod	4.48	0.00238	0.53
Total	1,092.67	0.06442	100