Assertion: fuselage's lift coefficient | /r/HasProperty | least 0.50
Facets:
Source sentences:
text: (ii) the fuselage lift coefficient is at least 0.50 at an angle of attack (α LZo ) of 10°, in level flight at sea level (ISA) with all moveable lift enhancing devices retracted.
text: (ii) the fuselage lift coefficient is at least 0.50 at an angle of attack (α LZo ) of 10°, in level flight at sea level (ISA) with all movable lift enhancing devices retracted.