1–6 von 6 Ergebnissen
|

    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

    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

    The Effects of Various Vortex Generator Configurations on a Normal Shock Wave / Boundary Layer Interaction

    Titchener, N. / Babinsky, H. / Loth, E. et al. | British Library Conference Proceedings | 2013

    Can Fundamental Shock-Wave/Boundary-Layer Interaction Research be Relevant to Inlet Aerodynamics?

    Titchener, N. / Babinsky, H. / Loth, E. et al. | British Library Conference Proceedings | 2012

    AN EXPERIMENTAL INVESTIGATION OF CORNER BLEED APPLIED TO A NORMAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION AND DIFFUSER

    Titchener, N. / Bruce, P. / Babinsky, H. et al. | British Library Conference Proceedings | 2011

    A Canonical Normal SBLI Flow Relevant to External Compression Inlets

    Loth, E. / Babinsky, H. / Titchener, N. et al. | British Library Conference Proceedings | 2013