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    A Parametric Study of the Blade Row Interaction in a High Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2009:;volume( 131 ):;issue: 003:;page 31006
    Author(s): G. Persico; P. Gaetani; C. Osnaghi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An extensive experimental analysis on the subject of the unsteady periodic flow in a high subsonic high pressure (HP) turbine stage has been carried out at the Laboratorio di Fluidodinamica ...
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    Unsteady Aerodynamics of a Low Aspect Ratio Turbine Stage: Modeling Issues and Flow Physics 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61030
    Author(s): G. Persico; A. Mora; M. Savini; P. Gaetani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper the three-dimensional unsteady aerodynamics of a low aspect ratio, high pressure turbine stage are studied. In particular, the results of fully unsteady three-dimensional numerical ...
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    Impeller-Vaned Diffuser Interaction in a Centrifugal Compressor at Off Design Conditions 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61034
    Author(s): P. Gaetani; G. Persico; A. Mora; V. Dossena; C. Osnaghi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As centrifugal compressors find a huge number of applications in industry and in aero-engines, the detailed analysis and comprehension of the impeller-vaned diffuser interaction is of interest ...
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    Three Dimensional Clocking Effects in a One and a Half Stage Transonic Turbine 

    Source: Journal of Turbomachinery:;2010:;volume( 132 ):;issue: 001:;page 11019
    Author(s): O. Schennach; B. Paradiso; G. Persico; J. Woisetschläger; P. Gaetani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental investigation of the flow field in a high-pressure transonic turbine with a downstream vane row (1.5 stage machine) concerning the airfoil indexing. The ...
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    Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part I: Three-Dimensional Time-Averaged Flow Field 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 572
    Author(s): P. Gaetani; G. Persico; V. Dossena; C. Osnaghi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An extensive experimental analysis on the subject of unsteady flow field in high-pressure turbine stages was carried out at the Laboratorio di Fluidodinamica delle Macchine (LFM) of Politecnico ...
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    Investigation of the Flow Field in a High-Pressure Turbine Stage for Two Stator-Rotor Axial Gaps—Part II: Unsteady Flow Field 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 003:;page 580
    Author(s): P. Gaetani; G. Persico; V. Dossena; C. Osnaghi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An extensive experimental analysis was carried out at Politecnico di Milano on the subject of unsteady flow in high pressure (HP) turbine stages. In this paper, the unsteady flow measured ...
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    Aerodynamic Measurements on a Vertical Axis Wind Turbine in a Large Scale Wind Tunnel 

    Source: Journal of Energy Resources Technology:;2011:;volume( 133 ):;issue: 003:;page 31201
    Author(s): L. Battisti; V. Dossena; G. Persico; L. Zanne; S. Dell’Anna; B. Paradiso
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the first results of a wide experimental investigation on the aerodynamics of a vertical axis wind turbine. Vertical axis wind turbines have recently received particular ...
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