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    Assessment of the Cold-Wire Resistance Thermometer for High-Speed Turbomachinery Applications 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 001:;page 140
    Author(s): R. Dénos; C. H. Sieverding
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper first describes the fundamentals of cold-wire resistance thermometry. The transfer functions with and without wire-prong heat conduction effects are discussed and a new method for the ...
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    Effect of the Hub Endwall Cavity Flow on the Flow-Field of a Transonic High-Pressure Turbine 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 578
    Author(s): G. Paniagua; R. Dénos; S. Almeida
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In high-pressure turbines, a small amount of cold flow is ejected at the hub from the cavity that exists between the stator and the rotor disk. This prevents the ingestion of hot gases into ...
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    Unsteady Rotor Heat Transfer in a Transonic Turbine Stage 

    Source: Journal of Turbomachinery:;2002:;volume( 124 ):;issue: 004:;page 614
    Author(s): F. Didier; R. Dénos; T. Arts
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This experimental investigation reports the convective heat transfer coefficient around the rotor of a transonic turbine stage. Both time-resolved and time-averaged aspects are addressed. The ...
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    Application of Hot-Wire Anemometry in a Blow-Down Turbine Facility 

    Source: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 002:;page 420
    Author(s): T. Yasa; G. Paniagua; R. Dénos
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to test HP turbine stages under engine representative conditions on a heat transfer point of view, blow-down test rigs are often used. In these rigs the evolution of gas temperature, ...
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    Investigation of the Unsteady Rotor Aerodynamics in a Transonic Turbine Stage 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 81
    Author(s): R. Dénos; V. Michelassi; F. Martelli; T. Arts; G. Paniagua
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper focuses on the unsteady pressure field measured around the rotor midspan profile of the VKI Brite transonic turbine stage. The understanding of the complex unsteady flow field is ...
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    Investigation of the Flow Field Downstream of a Turbine Trailing Edge Cooled Nozzle Guide Vane 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 002:;page 291
    Author(s): C. H. Sieverding; F. Martelli; T. Arts; R. Dénos
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A trailing edge cooled low aspect ratio transonic turbine guide vane is investigated in the VKI Compression Tube Cascade Facility at an outlet Mach number M 2, is = 1.05 and a coolant flow ...
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    Time-Averaged and Time-Resolved Heat Flux Measurements on a Turbine Stator Blade Using Two-Layered Thin-Film Gauges 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 004:;page 570
    Author(s): V. Iliopoulou; R. Dénos; N. Billiard; T. Arts
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the steps undertaken to measure heat flux in a turbine tested in a blowdown windtunnel when using a two-layered thin film gauge array. The sensor consists of a nickel ...
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    Unsteady Heat Transfer in Stator–Rotor Interaction by Two-Equation Turbulence Model 

    Source: Journal of Turbomachinery:;1999:;volume( 121 ):;issue: 003:;page 436
    Author(s): V. Michelassi; R. Dénos; T. Arts; F. Martelli; C. H. Sieverding
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A transonic turbine stage is computed by means of an unsteady Navier–Stokes solver. A two-equation turbulence model is coupled to a transition model based on integral parameters and an extra ...
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