P. N. Kuznetsov

Development of a numerical simulation methodology for propellers and ducted fans of transport unmanned aerial vehicles with a takeoff weight of 80 to 350 kg

For transport unmanned aerial vehicles, selecting propulsion characteristics is a key consideration. A distinction must be made between lift propulsors, which must provide sufficient thrust within limited dimensions, and cruise propulsors, which primarily require high efficiency in both hover and forward flight. The re...