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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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