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    Numerical Characterization of Aerodynamic Losses of Jet Arrays for Gas Turbine Applications 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 005:;page 52504
    Author(s): Antonio Andreini; Riccardo Da Soghe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Jet array is an arrangement typically used to cool several gas turbine parts. Some examples of such applications can be found in the impingement cooled region of gas turbine airfoils or in ...
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    Turbine Stator Well CFD Studies: Effects of Coolant Supply Geometry on Cavity Sealing Performance 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002:;page 21008
    Author(s): Antonio Andreini; Riccardo Da Soghe; Bruno Facchini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The increase of aeroengine performance through the improvement of aerodynamic efficiency of core flow is becoming more and more difficult to achieve. However, there are still some devices that ...
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    Analysis of Gas Turbine Rotating Cavities by a One-Dimensional Model: Definition of New Disk Friction Coefficient Correlations Set 

    Source: Journal of Turbomachinery:;2011:;volume( 133 ):;issue: 002:;page 21020
    Author(s): Riccardo Da Soghe; Bruno Facchini; Luca Innocenti; Mirko Micio
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Reliable design of a secondary air system is one of the main tasks for the safety and unfailing performance of gas turbine engines. To meet the increasing demands of gas turbine designs, ...
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