1–20 von 20 Ergebnissen
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    Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions

    Babinsky, H. / Li, Y. / Ford, C. W. Pitt | AIAA | 2009

    Normal-Shock/Boundary-Layer Interactions in Transonic Intakes at High Incidence

    Coschignano, A. / Babinsky, H. / Sheaf, C. et al. | AIAA | 2019

    NACA 0012 aerofoil in an oscillating transonic free-stream

    Fernie, R. / Babinsky, H. | AIAA | 2002

    Vortical Structures on Three-Dimensional Shock Control Bumps

    Colliss, S. P. / Babinsky, H. / Nübler, K. et al. | AIAA | 2016

    Joint Experimental and Numerical Approach to Three-Dimensional Shock Control Bump Research

    Colliss, S. P. / Babinsky, H. / Nübler, K. et al. | AIAA | 2014

    Experimental and Computational Investigations of a Normal-Hole-Bled Supersonic Boundary Layer

    Oorebeek, J. M. / Babinsky, H. / Ugolotti, M. et al. | AIAA | 2015

    Experimental and Numerical Study of Oscillating Transonic Shock Waves in Ducts

    Bruce, P. J. K. / Babinsky, H. / Tartinville, B. et al. | AIAA | 2011

    Corner Effect and Asymmetry in Transonic Channel Flows

    Bruce, P. J. K. / Babinsky, H. / Tartinville, B. et al. | AIAA | 2011

    Experiments and Computations on the Lift of Accelerating Flat Plates at Incidence

    Stevens, P. R. R. J. / Babinsky, H. / Manar, F. et al. | AIAA | 2017