The characteristic features of determination of aerodynamic descriptions of беспилотного LA are considered with an additional bearing surface is a hybrid bearing chart (GNS). The method of determination of coefficients of carrying capacity and resistance of BPLA is offered with GNS on the basis of panel-vortical method. The analysis of influencing of parameters of arrangement is executed on calculation aerodynamic descriptions.
aerodynamic chart, additional bearings surfaces, experiment, model, fuselage, covered, flight-landings descriptions
"Raschetnaia otsenka aэrodynamycheskykh kharakterystyk BPLA s hybrydnoi nesushchei skhemoi" ,
Scientific Works of Kharkiv National Air Force University,