1–15 von 15 Ergebnissen
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    FOURTH ORDER

    KRAUSE, E / HIRSCHEL, E / KORDULLA, W | AIAA | 1973

    Vortex-dominated flow with viscous core structure

    LIU, C. / KRAUSE, E. / TING, L. | AIAA | 1985

    Admissible upstream conditions for slender compressible vortices

    LIU, C. / KRAUSE, E. / MENNE, S. | AIAA | 1986

    Numerical simulation of laminar hypersonic shock-boundary layer interaction

    Domröse, U. / Krause, E. / Meinke, M. | Tema Archiv | 1996

    Computation of leading edge vortices

    KRAUSE, E. / SHI, X.-G. / HARTWICH, P.-M. | AIAA | 1983

    Investigation of vortex structures on delta wings

    Stromberg, A. / Henze, A. / Limberg, W. et al. | Tema Archiv | 1996

    In-flight measuring techniques for laminar flow wing development

    Ewald, B. / Durst, F. / Krause, E. et al. | Tema Archiv | 1993

    Cycle-resolved computations of compressible flow in engine

    Naitoh,K. / Ono,M. / Kuwahara,K. et al. | Kraftfahrwesen | 2002

    Recent progress in hypersonics: the ELAC configuration

    Krause, E. / Henze, A. / European Space Agency et al. | British Library Conference Proceedings | 1995