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    A Novel Mixing Plane Method Using Nonreflecting Boundary Conditions for Multirow Analysis in Turbomachines 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 007:;page 71009
    Author(s): Gisbert, Fernando; Corral, Roque
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A new formulation of the mixing plane boundary condition to analyze the steadystate interaction between adjacent rows of a turbomachine, used in conjunction with steady twodimensional nonreflecting boundary conditions, is ...
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    Prediction of Reynolds Number Effects on Low-Pressure Turbines Using a High-Order ILES Method 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 003
    Author(s): Bolinches-Gisbert, M.; Robles, David Cadrecha; Corral, Roque; Gisbert, Fernando
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A comprehensive comparison between implicit large eddy simulations (ILES) and experimental results of a modern high-lift low-pressure turbine airfoil has been carried out for an array of Reynolds numbers (Re). Experimental ...
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    Numerical and Experimental Investigation of the Reynolds Number and Reduced Frequency Effects on Low-Pressure Turbine Airfoils 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 002:;page 021004-1
    Author(s): Bolinches-Gisbert, M.; Robles, David Cadrecha; Corral, Roque; Gisbert, Fernando
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This article compares experimental and numerical data for a low-speed high-lift low pressure turbine (LPT) cascade under unsteady flow conditions. Three Reynolds numbers representative of LPTs have been tested, namely, 5 ...
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