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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Flight Mechanics of Rotor Aircraft . Flugmechanik der Drehfluegelflugzeuge


    Publication date :

    1971


    Size :

    127 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English