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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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    The Effect of Size on Optimization of Solid Oxide Fuel Cell/Gas Turbine Hybrid Cycles 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 009:;page 94502
    Author(s): Michael J. Brear; Michael J. Dunkley
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The coupling of solid oxide fuel cells (SOFCs) and recuperated gas turbines (GTs) in a hybrid system has the potential to lead to efficiencies exceeding 60%. SOFC/GT hybrids have been proposed ...
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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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    Propulsion System Requirements for Long Range, Supersonic Aircraft 

    Source: Journal of Fluids Engineering:;2006:;volume( 128 ):;issue: 002:;page 370
    Author(s): Michael J. Brear; Jack L. Kerrebrock; Alan H. Epstein
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the requirements for the propulsion system of supersonic cruise aircraft that are quiet enough to fly over land and operate from civil airports, have trans-pacific range ...
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    Flow Separation Within the Engine Inlet of an Uninhabited Combat Air Vehicle (UCAV) 

    Source: Journal of Fluids Engineering:;2004:;volume( 126 ):;issue: 002:;page 266
    Author(s): Michael J. Brear; Zachary Warfield; John F. Mangus; Steve Braddom; James D. Paduano; Jeffry S. Philhower
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper discusses the structure of the flow within the engine inlet of an uninhabited combat air vehicle (UCAV). The UCAV features a top-mounted, serpentine inlet leading to an engine buried ...
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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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