Assertion: fuselage's lift coefficient | /r/HasProperty | least 0.60
Facets:
Source sentences:
text: Another object of the invention is to provide an aircraft in which (a) the fuselage lift coefficient is 0.03 or less at an altitude between 25,000 and 51,000 ft. ISA in level flight at a speed of 0.5 to 0.95 IMN, while at minimum calibrated airspeed in level flight at sea level ISA, the fuselage lift coefficient (CL F ) is at least 0.60, preferably 0.70 to 4.0.