Author presents principles for design of helicopter, based on forced procession; analysis given explains how normal reaction torque, when it has been countered by forcibly contra-processing spinning rotor, reappears as revolving horizontal traction and revolving overturning moment; principle and mechanism explained and illustrated.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Single-rotor helicopter without reaction torque


    Weitere Titelangaben:

    Aeronautical Eng Rev


    Beteiligte:
    Collins, T. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1944


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Ornicopter Yaw Control: Testing a Single Rotor Helicopter Without Reaction Torque

    van Gerwen, Dennis / van Holten, Theo / Heiligers, Monique | AIAA | 2007


    Power system of single-rotor helicopter without reactive torque tail rotor

    WANG ZEMIN | Europäisches Patentamt | 2021

    Freier Zugriff

    Ornicopter Yaw Control: Testing a Single Rotor Helicopter Without Reaction Torque AIAA Paper

    van Gerwen, D. / van Holten, T. / Heiligers, M. et al. | British Library Conference Proceedings | 2007


    Development of a Radio-Controlled Ornicopter: a Single Rotor Helicopter Without Reaction Torque

    Heiligers, Monique / Kuiper, Rolf / van den Bulcke, Stijn et al. | SAE Technical Papers | 2005


    Development of a Radio-Controlled Ornicopter: a Single Rotor Helicopter Without Reaction Torque

    Heiligers, M. / Kuiper, R. / von Holten, T. et al. | British Library Conference Proceedings | 2005