airfoil primary subject, 11 assertions
There are no subgroups or aspects for airfoil in Ascent++.
CapableOf 2
produce lift 0.84
move with the wind 0.44
HasA 4
an angle of attack 0.41
chord reference plane 0.35
rigid mid 0.25
current fairings 0.25
HasProperty 2
thin 0.41
symmetrical 0.38
ReceivesAction 3
positioned in a high-dr… 0.31
inclined 0.25
clocked 0.25