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    The Effect of Wake Passing on a Flow Separation in a Low-Pressure Turbine Cascade 

    Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 002:;page 250
    Author(s): Michael J. Brear; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an investigation into the effect that passing wakes have on a separation bubble that exists on the pressure surface and near the leading edge of a low-pressure turbine ...
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    Transition on the T106 LP Turbine Blade in the Presence of Moving Upstream Wakes and Downstream Potential Fields 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 004:;page 41017
    Author(s): Maciej M. Opoka; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Boundary layer measurements were performed on a cascade of the T106 high lift low-pressure (LP) turbine blades that was subjected to upstream wakes and a moving downstream potential field. Tests ...
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    Boundary Layer Transition on the High Lift T106A Low-Pressure Turbine Blade With an Oscillating Downstream Pressure Field 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 002:;page 21009
    Author(s): Maciej M. Opoka; Richard L. Thomas; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of an experimental study of the interaction between the suction surface boundary layer of a cascade of low-pressure (LP) turbine blades and a fluctuating downstream ...
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    The Effect of Wake Induced Structures on Compressor Boundary-Layers 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 004:;page 705
    Author(s): Andrew P. Wheeler; Robert J. Miller; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The interaction of a convected wake with a compressor blade boundary layer was investigated. Measurements within a single-stage compressor were made using an endoscopic PIV system, a surface ...
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    A New Intermittent Aspirated Probe for the Measurement of Stagnation Quantities in High Temperature Gases 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 004:;page 41022
    Author(s): Michela Massini; Robert J. Miller; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the design, manufacture, and testing of a new probe for the measurement of temperature and pressure in engine environments. The probe consists of a choked nozzle located ...
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    Pressure Surface Separations in Low-Pressure Turbines—Part 1: Midspan Behavior 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 393
    Author(s): Michael J. Brear; Neil W. Harvey; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes an investigation into the behavior of the pressure surface separation at midspan in a linear cascade. It is found that the pressure surface separation can be a significant ...
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    Optimization of Nonaxisymmetric Endwalls in Compressor S-Shaped Ducts 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11011
    Author(s): Edward M. J. Naylor; Cecilia Ortiz Dueñas; Robert J. Miller; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a new design methodology for strutted S-shaped compressor ducts that allows for more aggressive designs while maintaining current levels of duct loss. A baseline duct geometry ...
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    A New Alternative for Reduction in Secondary Flows in Low Pressure Turbines 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 001:;page 11029
    Author(s): Diego Torre; Raúl Vázquez; Elena de la Rosa Blanco; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a new flow mechanism for the reduction in secondary flows in low pressure turbines using the benefit of contoured endwalls. The extensive application of contoured endwalls ...
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    Pressure Surface Separations in Low-Pressure Turbines—Part 2: Interactions With the Secondary Flow 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 003:;page 402
    Author(s): Michael J. Brear; Paloma Gonzalez; Neil W. Harvey; Howard P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a study of the interaction between the pressure surface separation and the secondary flow on low-pressure turbine blades. It is found that this interaction can significantly ...
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