Assertion: fuselage's lift coefficient | /r/CapableOf | apply general formula
Facets:
value: as the reference area
type: OTHER
Source sentences:
text: The wing lift coefficient (C LW ) of this invention is calculated by measuring total wing lift (again with flaps not deployed and attributing carryover lift to the fuselage only), and applying the general formula using (S w ) as the reference area.
text: The wing lift coefficient (C LV ) of this invention is calculated by measuring total wing lift (again with flaps not deployed and attributing carryover lift to the fuselage only), and applying the general formula using (S w ) as the reference area.