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    Experimental Investigation on the Time–Space Evolution of a Laminar Separation Bubble by Proper Orthogonal Decomposition and Dynamic Mode Decomposition 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 003:;page 31006
    Author(s): Lengani, D.; Simoni, D.; Ubaldi, M.; Zunino, P.; Bertini, F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A time-resolved particle image velocimetry (TR-PIV) system has been employed to investigate a laminar separation bubble which is induced by a strong adverse pressure gradient typical of ultrahigh-lift low-pressure turbine ...
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    Effects of Ribbed Surfaces on Profile Losses of Low-Pressure Turbine Blades 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 010:;page 101009-1
    Author(s): Dellacasagrande, M.; Lengani, D.; Simoni, D.; Ubaldi, M.; Bertini, F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this work, streamwise oriented riblets were installed on a flat plate exposed to an adverse pressure gradient typical of low-pressure turbine (LPT) blade and, successively, on the suction side of an LPT cascade operating ...
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    On the Identification and Decomposition of the Unsteady Losses in a Turbine Cascade 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 003:;page 31005
    Author(s): Lengani, D.; Simoni, D.; Pichler, R.; Sandberg, R. D.; Michelassi, V.; Bertini, F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present paper describes the application of proper orthogonal decomposition (POD) to large eddy simulation (LES) of the T106A low-pressure-turbine profile with unsteady incoming wakes at two different flow conditions. ...
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    Recognition of Structures Leading to Transition in a Low-Pressure Turbine Cascade: Effect of Reduced Frequency 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 006:;page 061007-1
    Author(s): Lengani, D.; Simoni, D.; Ubaldi, M.; Zunino, P.; Bertini, F.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The boundary layer developing over the suction side of a low-pressure turbine cascade operating under unsteady inflow conditions has been experimentally investigated. Time-resolved particle image velocimetry (PIV) measurements ...
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