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    The Influence of Endwall Contouring on the Performance of a Turbine Nozzle Guide Vane 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 002:;page 200
    Author(s): V. Dossena; A. Perdichizzi; M. Savini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents the results of a detailed investigation of the flow field in a gas turbine linear cascade. A comparison between a contoured and a planar configuration of the same cascade ...
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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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    Secondary Flows in a Transonic Cascade: Comparison Between Experimental and Numerical Results 

    Source: Journal of Fluids Engineering:;1989:;volume( 111 ):;issue: 004:;page 369
    Author(s): F. Bassi; C. Osnaghi; A. Perdichizzi; M. Savini
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper presents a comparison between numerical results and experimental data about the secondary flow development in a linear transonic turbine cascade. Computations are carried out by using ...
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