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    Gas Turbine Combined Cycle Optimized for Postcombustion Carbon Capture 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 009:;page 91701
    Author(s): Can Gülen, S.; Hall, Chris
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes a gas turbine combined cycle (GTCC) power plant system, which addresses the three key design challenges of postcombustion CO2 capture from the stack gas of a GTCC power plant using aqueous amine-based ...
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    An Experimental, Aerodynamic Evaluation of Design Choices for a Low-Pressure Compressor Transition Duct 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091004-1
    Author(s): Walker, A. Duncan; Mariah, Ian; Hall, Chris
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The S-shaped duct which transfers flow from the low-pressure fan to the engine core in large civil turbofans presents a challenging problem. Aerodynamically it has a spatially and temporarily varying inlet flow combined ...
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    The Influence of Fan Root Flow on the Aerodynamic of a Low-Pressure Compressor Transition Duct 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 001:;page 011002-1
    Author(s): Walker, A. Duncan; Mariah, Ian; Tsakmakidou, Dimitra; Vadhvana, Hiren; Hall, Chris
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: To reduce fuel-burn and emissions, there is a drive toward higher bypass ratio and smaller high-pressure ratio core engines. This makes the design of the ducts connecting compressor spools more challenging as the higher ...
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    Experimental Investigation of Secondary Flows and Length Reduction for a Low-Pressure Compressor Transition Duct 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 144 ):;issue: 001:;page 11017-1
    Author(s): Tsakmakidou, Dimitra; Mariah, Ian; Walker, A. Duncan; Hall, Chris; Simpson, Harry
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The need to reduce fuel-burn and emissions is pushing turbofan engines toward geared architectures with higher bypass ratios and small ultrahigh-pressure ratio cores. However, this increases the radial offset between ...
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