Prominent features of definition of integrated aerodynamic characteristics pilotless aircrafts with a wing of parachute type are considered. The technique of definition of factors of elevating force and resistance pilotless aircrafts with an aeroelastic wing is offered. It is made the analysis of influence of parameters of configuration on settlement aerodynamic characteristics.
paraplan, experiment, model, calculation of fuselage, covered, flight, landing
"Vplyv parametriv komponuvannia BPLA z parakrylom na yoho aerodynamichni kharakterystyky" ,
Scientific Works of Kharkiv National Air Force University,