A theoretical investigation comparing the yaw maneuverability of various types of helicopters is reported. Calculation of the behavior of helicopters in autorotation is described. The simulation of a tied down helicopter by means of a hybrid computer is treated. Two exact theories for rotor wake calculations are compared.
Flight Mechanics of Rotor Aircraft . Flugmechanik der Drehfluegelflugzeuge
1971
127 pages
Report
Keine Angabe
Englisch