1–3 of 3 hits
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    Numerical simulation of helicopter aeromechanics in slow descent flight

    Embacher, M. / Keßler, M. / Bensing, F. et al. | Tema Archive | 2009
    BVI induced airloads. In contrast to earlier results, the vortex grids are extended to fill the entire rotor disk and the trim including the ...

    Wing-tip vortex / jet interaction in the extended near field

    Zurheide, Frank T. / Meinke, Matthias / Schröder, Wolfgang | Tema Archive | 2009
    . Results from wind tunnel measurements are used as inflow boundary conditions for an LES of the wake region. An aircraft engine is modeled in the ...

    Aeroacoustic prediction of jet and slat noise

    Gröschel, E. / König, D. / Koh, S. et al. | Tema Archive | 2008
    The flow field and the acoustic field of various jet flows and a high-lift configuration consisting of a deployed slat and a main wing are ...