Assertion: fuselage | /r/CapableOf | generate 50%-100% of the lift
Facets:
Source sentences:
text: If the angle of incidence is set at 6° the wing may be partially or fully stalled when the fuselage is pitched up to α ZLo =12°, and the fuselage may be generating 50%-100% of the lift, while its lift coefficient, C LF , is at least 0.6 and preferably 0.80 to 1.8, measured with high-lift devices retracted.