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    Modeling of Film Cooling—Part I: Experimental Study of Flow Structure 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 001:;page 141
    Author(s): Stefan Bernsdorf; Martin G. Rose; Reza S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper, which is Part I of a two part paper, reports on experimental data taken in a steady flow, flat plate wind tunnel at ETH Zürich, while Part II utilizes this data for ...
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    Modeling of Film Cooling—Part II: Model for Use in Three-Dimensional Computational Fluid Dynamics 

    Source: Journal of Turbomachinery:;2007:;volume( 129 ):;issue: 002:;page 221
    Author(s): André Burdet; Reza S. Abhari; Martin G. Rose
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Computational fluid dynamics (CFD) has recently been used for the simulation of the aerothermodynamics of film cooling. The direct calculation of a single cooling hole requires substantial ...
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    Experimental Validation of Quasisteady Assumption in Modeling of Unsteady Film-Cooling 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001:;page 11022
    Author(s): Stefan Bernsdorf; Martin G. Rose; Reza S. Abhari
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper reports on the validation of the assumption of quasisteady behavior of pulsating cooling injection in the near hole flow region. The respective experimental data are taken in a flat ...
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    Low Pressure Turbine Secondary Vortices: Reynolds Lapse 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 006:;page 61022
    Author(s): Matthias Kuerner; Daniel Schrack; Jochen Gier; Karl Engel; Martin G. Rose; Georg A. Reichstein; Stephan Staudacher
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A two-stage turbine is tested in a cooperation between the Institute of Aircraft Propulsion Systems (ILA) and MTU Aero Engines GmbH (MTU). The experimental results taken in the Altitude Test ...
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    Nonaxisymmetric Turbine End Wall Design: Part I— Three-Dimensional Linear Design System 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 002:;page 278
    Author(s): Neil W. Harvey; Shahrokh Shahpar; Jonathan Hartland; David G. Gregory-Smith; Martin G. Rose; Mark D. Taylor
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A linear design system, already in use for the forward and inverse design of three-dimensional turbine aerofoils, has been extended for the design of their end walls. This paper shows how ...
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