Assertion: airfoil's center | /r/CapableOf | lie at maximum lift coefficient
Facets:
value: for a reflex-cambered airfoil
type: TRANSITIVE-OBJECT
Source sentences:
text: For a reflex-cambered airfoil, the center of pressure lies a little ahead of the quarter-chord point at maximum lift coefficient (large angle of attack), but as lift coefficient reduces (angle of attack reduces) the center of pressure moves forward.