Search Results - "Bruce, Paul J. K."

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  1. 1

    On the Formation Mechanisms of Artificially Generated High Reynolds Number Turbulent Boundary Layers by Rodríguez-López, Eduardo, Bruce, Paul J. K., Buxton, Oliver R. H.

    Published in Boundary-layer meteorology (01-08-2016)
    “…We investigate the evolution of an artificially thick turbulent boundary layer generated by two families of small obstacles (divided into uniform and…”
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  2. 2

    A robust post-processing method to determine skin friction in turbulent boundary layers from the velocity profile by Rodríguez-López, Eduardo, Bruce, Paul J. K., Buxton, Oliver R. H.

    Published in Experiments in fluids (01-04-2015)
    “…The present paper describes a method to extrapolate the mean wall shear stress, τ w a l l , and the accurate relative position of a velocity probe with respect…”
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  3. 3

    Photogrammetry for accurate model deformation measurement in a supersonic wind tunnel by Gramola, Michela, Bruce, Paul J. K., Santer, Matthew

    Published in Experiments in fluids (2019)
    “…The interest in adaptive devices for high-speed applications leads to the need for an accurate and reliable technique to obtain model deformation measurements…”
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  4. 4

    Experimental characterization of the hypersonic flow around a cuboid by Rees, Thomas W., Fisher, Tom B., Bruce, Paul J. K., Merrifield, Jim A., Quinn, Mark K.

    Published in Experiments in fluids (2020)
    “…Understanding the hypersonic flow around faceted shapes is important in the context of the fragmentation and demise of satellites undergoing uncontrolled…”
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  5. 5

    Correction to: Experimental characterization of the hypersonic flow around a cuboid by Rees, Thomas W., Fisher, Tom B., Bruce, Paul J. K., Merrifield, Jim A., Quinn, Mark K.

    Published in Experiments in fluids (2020)
    “…There is a typographical error in Equation 13, which should instead read:…”
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  6. 6

    Numerical and experimental studies of the hypersonic flow around a cube at incidence by Rees, Thomas W., Bruce, Paul J.K., Fisher, Tom B., Quinn, Mark K., Merrifield, Jim A.

    Published in Acta astronautica (01-06-2021)
    “…In order to improve predictions of the on-ground casualty risk associated with the uncontrolled atmospheric re-entry of satellites from Low Earth Orbit, there…”
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  7. 7

    Experimental measurement of wall shear stress in strongly disrupted flows by Rodríguez-López, Eduardo, Bruce, Paul J.K., Buxton, Oliver R.H.

    Published in Journal of turbulence (04-03-2017)
    “…Mean and fluctuating wall shear stress is measured in strongly disrupted cases generated by various low-porosity wall-mounted single- and multi-scale fences…”
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  8. 8

    Passive control of 3D adaptive shock control bumps using a sealed cavity by Gramola, Michela, Bruce, Paul J.K., Santer, Matthew

    Published in Journal of fluids and structures (01-07-2022)
    “…This paper presents a Fluid–Structure-Interaction study of a novel passive adaptive shock control bump concept. A flexible plate, clamped on all sides and…”
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  9. 9

    Off-design performance of 2D adaptive shock control bumps by Gramola, Michela, Bruce, Paul J.K., Santer, Matthew

    Published in Journal of fluids and structures (01-02-2020)
    “…Adaptive shock control bumps can exploit the on-design drag-reducing potential of 2D bumps, while mitigating their off-design performance deterioration through…”
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  10. 10

    Experimental FSI study of adaptive shock control bumps by Gramola, Michela, Bruce, Paul J.K., Santer, Matthew

    Published in Journal of fluids and structures (01-08-2018)
    “…The shock stabilisation and wave drag reduction potential of a two-dimensional adaptive shock control bump has been studied in the Imperial College supersonic…”
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  11. 11
  12. 12

    Aerothermodynamic Analysis of Faceted Aeroshell at Hypersonic Speed by Innocenzi, Pietro, Gramola, Michela, Fisher, Tom B, Quinn, Mark K, Bruce, Paul J. K, Navarro-Martinez, Salvador

    Published 22-11-2023
    “…This study explores the aerothermal behaviour of a rigid mechanically deployable aeroshell developed at Imperial College London for high payload atmospheric…”
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