Assertion: airfoil's drag | /r/CapableOf | increase the angle of attack of c l m
Facets:
Source sentences:
text: Induced drag effectively reduces the slope of the lift curve of a 2-D airfoil and increases the angle of attack of C L m a x {\displaystyle C_{L_{max}}} C L m a x {\displaystyle C_{L_{max}}}