Contributed paper Selected aerodynamic Design issues for the single-rotor remotely Piloted helicopter

摘要

Some of the fundamental problems associated with the aerodynamic configuration of a single-rotor remotely piloted helicopter are discussed in this paper. A method for selecting the aerodynamic shape of a fuselage and determining the locations and parameters of a horizontal stabilizer and a tail rotor in the preliminary design analysis is given. The application of this method to a remotely piloted single main rotor and tail rotor helicopter developed at the Nanjing University of Aeronautics and Astronautics is described.