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1–12 von 12 Ergebnissen
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    Methods for the prediction of blade-vortex interaction noise

    Caradonna, F. / Kitaplioglu, C. / McCluer, M. et al. | Tema Archiv | 2000
    Schlagwörter: mathematisches Modell

    Theoretical and experimental study of unsteady rotor/body aerodynamic interactions

    Crouse, G.L. jun. / Leishman, J.G. / Bi, N. | Tema Archiv | 1992
    Schlagwörter: RECHENMODELL

    Rotor free-wake modeling using a relaxation technique - including comparisons with experimental data

    Bagai, A. / Leishman, J.G. | Tema Archiv | 1994
    Schlagwörter: Rechenmodell

    Rotor aerodynamics during maneuvering flight using a time-accurate free-vortex wake

    Bhagwat, M.J. / Leishman, J.G. | Tema Archiv | 2003
    Schlagwörter: mathematisches Modell

    Sound directivity generated by helicopter rotors using wave tracing concepts

    Leishman, J.G. | Tema Archiv | 1999
    Schlagwörter: Rechenmodell

    Analysis of pitch and plunge effects on unsteady airfoil behavior

    Tyler, J.C. / Leishman, J.G. | Tema Archiv | 1992
    Schlagwörter: Rechenmodell

    A semi-empirical model for dynamic stall

    Leishman, J.G. / Beddoes, T.S. | Tema Archiv | 1989
    Schlagwörter: RECHENMODELL

    Rotor free-wake modeling using a pseudo-implicit technique - Including comparisons with experimental data

    Bagai, A. / Leishman, J.G. | Tema Archiv | 1995
    Schlagwörter: Rechenmodell

    Modeling sweep effects on dynamic stall

    Leishman, J.G. | Tema Archiv | 1989
    Schlagwörter: RECHENMODELL

    Effects of unsteady blowing on the lift of a circulation controlled cylinder

    Ghee, T.A. / Leishman, J.G. | Tema Archiv | 1990
    Schlagwörter: RECHENMODELL

    Modeling of subsonic unsteady aerodynamics for rotary wing applications

    Leishman, J.G. | Tema Archiv | 1990
    Schlagwörter: RECHENMODELL

    Measurements of rotor tip vortices using three-component laser Doppler velocimetry

    Leishman, J.G. / Baker, A. / Coyne, A. | Tema Archiv | 1996
    Schlagwörter: Rechenmodell