One of problems facing designer of rotary wing aircraft is that of determining blade aerodynamic loading, in particular oscillatory content of this loading; using simple downwash theories, and placing blade in flapping equilibrium, it is possible to compute helicopter airloads corresponding to velocity change; simplified treatment of shed wake and application of theory presented.


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    Titel :

    On computation of airloads acting on rotor blades in forward flight


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Miller, R.H. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    11 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Analysis of High Resolution Unsteady Airloads for Helicopter Rotor Blades

    Quackenbush, T. R. / Lam, C.-M. G. / Wachpress, D. A. et al. | British Library Conference Proceedings | 1994


    Analysis of high resolution unsteady airloads for helicopter rotor blades

    Quackenbush, T.R. / Lam, C.M.G. / Wachspress, D.A. et al. | Tema Archiv | 1994


    UH-60A helicopter rotor airloads measured in flight

    Kufeld, R.M. | Online Contents | 1997



    Forward Flight Rotor Airloads Predictions using a Coupled Navier-Stokes/Full-Potential Analysis

    Berezin, C. / Sankar, L. N. / Advisory Group for Aerospace Research and Development et al. | British Library Conference Proceedings | 1995