Outline of methods for calculating response of rotary wing airplanes to arbitrary control displacements. Before Inst Aeronautical Sciences.


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    Title :

    Response of helicopters with articulated rotors to cyclic blade pitch control


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Donovan, A.F. (author) / Goland, M. (author)


    Publication date :

    1944


    Size :

    11 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    The Effects of Blade Flexibility on the Control Response of an Articulated-Rotor Helicopters

    Kothmann, B. D. / Curtiss, H. C. | British Library Conference Proceedings | 1995


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    Ramos, R. / de Andrade, D. / Goes, L.C. et al. | British Library Conference Proceedings | 2009


    Recent studies of pitch-lag instabilities of articulated rotors

    Blake, B.B. / Burkam, J.E. / Loewy, R.G. | Engineering Index Backfile | 1961