1–50 von 114 Ergebnissen
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    An Experimental Study on Truck Side-Skirt Flow

    Babinsky, H. / Stephens, R.G. | SAE Technical Papers | 2016

    Microramp Control of Supersonic Oblique Shock-Wave/Boundary-Layer Interactions

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

    Evaluation of wave drag reduction by flow control

    Ogawa, H. / Babinsky, H. | Elsevier | 2005

    The aerodynamic performance of paragliders

    Babinsky, H. | Online Contents | 1999

    Shock-Wave/Boundary-Layer Interaction Control Using Three-Dimensional Bumps for Transonic Wings

    Ogawa, H. / Babinsky, H. / Pätzold, M. et al. | AIAA | 2008

    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

    An experimental study on truck side-skirt flow

    Stephens,R.G. / Babinsky,H. / Cambridge Univ.,US | Kraftfahrwesen | 2015

    Vortical Structures on Three-Dimensional Shock Control Bumps

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

      Vortical Structures on Three-Dimensional Shock Control Bumps

      Colliss, S. P | Online Contents | 2016
      Beteiligte: Babinsky, H

      Vortical Structures on Three-Dimensional Shock Control Bumps

      Colliss, S. P | Online Contents | 2016
      Beteiligte: Babinsky, H

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

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

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

      Colliss, S P | Online Contents | 2014
      Beteiligte: Babinsky, H

    A combined experimental and numerical study of flow structures over three-dimensional shock control bumps

    Wong, W.S. / Qin, N. / Sellars, N. et al. | Elsevier | 2007

    Bleed and Vortex Generator Effectiveness for Separation Prevention in a Transonic Diffuser (AIAA 2014-2793)

    Oorebeek, J. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Low Reynolds Number Experimental Studies on Flat Plates (AIAA 2014-0743)

    Stevens, R.J. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    Unsteady Shock Behaviour on a NACA0012 Aerofoil

    Fernie, R. M. / Babinsky, H. / AIAA | British Library Conference Proceedings | 2003

    An Investigation of Interactions between Normal Shocks and Transitional Boundary Layers

    Davidson, T. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2014

    2012-2812 Comparison of Micro-Vortex Generators in Supersonic Flows

    Nolan, W. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Flow Physics of a Normal-hole Bled Supersonic Turbulent Boundary Layer

    Oorebeek, J. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2013

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

      Oorebeek, J. M | Online Contents | 2015
      Beteiligte: Babinsky, H

    Control of a Shock-Wave/Boundary-Layer Interaction and Subsequent Subsonic Diffuser Using a Combination of Vortex Generators and Bleed

    Titchener, N. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Lift and the Leading Edge Vortex

    Ford, C.P. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    Normal Shock Interactions in Rectangular Channels

    Burton, D. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012

    AN EXPERIMENTAL STUDY INTO THE FLOW PHYSICS OF THREE-DIMENSIONAL SHOCK CONTROL BUMPS

    Bruce, P. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    CHARACTERIZATION OF MICRO-VORTEX GENERATORS IN SUPERSONIC FLOWS

    Nolan, W. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    LEADING EDGE VORTEX DEVELOPMENT ON A WAVING WING AT REYNOLDS NUMBERS BETWEEN 10,000 AND 60,000

    Jones, A. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    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

      Corner Effect and Asymmetry in Transonic Channel Flows

      Bruce, P J K | Online Contents | 2011
      Beteiligte: Babinsky, H

    LOW REYNOLDS NUMBER EXPERIMENTS ON AN IMPULSIVELY STARTED FLAT PLATE AT HIGH INCIDENCE

    Ford, C.P. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2011

    MICRO-VORTEX GENERATORS APPLIED TO A FLOW-FIELD CONTAINING A NORMAL SHOCK-WAVE AND DIFFUSER

    Titchener, N. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Behaviour of Unsteady Transonic Shock/Boundary Layer Interactions with Three-Dimensional Effects

    Bruce, P. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    THREE-DIMENSIONAL EFFECTS ON A WAVING WING

    Jones, A. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2010

    Leading Edge Flaps at Low Reynolds Numbers

    Jones, A. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2008

    Quantitative Heat Transfer Measurement using Liquid Crystal Thermography in an Hypersonic Gun Tunnel

    Babinsky, H. / Edwards, J. A. / IUTAM | British Library Conference Proceedings | 1994

    Impulsively Started Flat Plate Wing

    Beckwith, R. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    A Representative Flowfield of External Compression Inlets and Diffusers

    Loth, E. / Babinsky, H. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009

    The Effect of Tunnel Size on Incident Shock Boundary Layer Interaction Experiments

    Benek, J. / Suchyta, C. / Babinsky, H. et al. | British Library Conference Proceedings | 2013