Assertion: fuselage's lift coefficient | /r/HasProperty | small
Facets:
value: at the chosen cruise design point
type: LOCATION
Source sentences:
text: For this reason the lift coefficient of the fuselage is small at the chosen cruise design point, but not zero, unless positive lift from the fuselage happens to be exactly cancelled by a down force produced at the rear for trim or stability purposes.
text: For this reason the lift coefficient of the fuselage is small at the chosen cruise design point, but not zero, unless positive lift from the fuselage happens to be exactly cancelled by a down force produced at the rear for trim or stability purposes.