Flight-test program conducted with helicopter having power control system to determine what control forces would be desirable for various modes of flight; six different configurations were evaluated; evaluation was purely qualitative, made up of opinion of eight research pilots; feel spring of 1/2 lb/in. and bobweight of 14 lb/g provided desirable control feel forces.


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    Titel :

    Flight evaluation of several spring force gradients and bobweight in cyclic-power-control system of light helicopter


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Mallick, D.L. (Autor:in) / Reeder, J.P. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Model helicopter flight control

    Staiger, S. / Lehmann, R. / Schröder, W. | Tema Archiv | 2009


    Integrated Helicopter Flight Control

    J. A. Stephens / R. J. Kibler | NTIS | 1976


    Flight Test Evaluation of a Nonlinear Hub Spring on a UH-1H Helicopter

    P. J. Hollifield / L. W. Dooley / J. R. Van Gaasbeek et al. | NTIS | 1981