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    Developments in Hot-Streak Simulators for Turbine Testing 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 003:;page 31009
    Author(s): Thomas Povey; Imran Qureshi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The importance of understanding the impact of hot-streaks, and temperature distortion in general, on the high pressure turbine is widely appreciated, although it is still generally the case that ...
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    Effect of Simulated Combustor Temperature Nonuniformity on HP Vane and End Wall Heat Transfer: An Experimental and Computational Investigation 

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 003:;page 31901
    Author(s): Imran Qureshi; Arrigo Beretta; Thomas Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents experimental measurements and computational predictions of surface and end wall heat transfer for a high-pressure (HP) nozzle guide vane operating as part of a full HP turbine ...
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    Effect of Temperature Nonuniformity on Heat Transfer in an Unshrouded Transonic HP Turbine: An Experimental and Computational Investigation 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 001:;page 11005
    Author(s): Imran Qureshi; Andy D. Smith; Kam S. Chana; Thomas Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Detailed experimental measurements have been performed to understand the effects of turbine inlet temperature distortion (hot-streaks) on the heat transfer and aerodynamic characteristics of a ...
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    Effect of Aggressive Inlet Swirl on Heat Transfer and Aerodynamics in an Unshrouded Transonic HP Turbine 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61023
    Author(s): Imran Qureshi; Arrigo Beretta; Kam Chana; Thomas Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Swirling flows are now widely being used in modern gas turbine combustors to improve the combustion characteristics, flame stability, and reduce emissions. Residual swirl at the combustor exit ...
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    Analysis on the Effect of a Nonuniform Inlet Profile on Heat Transfer and Fluid Flow in Turbine Stages 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 001:;page 11012
    Author(s): Salvadori Simone; Francesco Montomoli; Francesco Martelli; Kam S. Chana; Imran Qureshi; Tom Povey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an investigation of the aerothermal performance of a modern unshrouded high-pressure (HP) aero-engine turbine subject to nonuniform inlet temperature profile. The turbine used ...
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