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    Experimental Investigation of Pressure Side Flow Separation on the T106C Airfoil at High Suction Side Incidence Flow 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 005:;page 51007
    Author(s): Stotz, Stephan; Guendogdu, Yavuz; Niehuis, Reinhard
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this work is to study the influence of a pressure side separation bubble on the profile losses and the development of the bubble in the blade passage. For the experimental investigations, the T106 profile ...
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    Boundary Layer Control on a Low Pressure Turbine Blade by Means of Pulsed Blowing 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51023
    Author(s): Mack, Marion; Niehuis, Reinhard; Fiala, Andreas; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current work investigates the performance benefits of pulsed blowing with frequencies up to 10 kHz on a highly loaded low pressure turbine (LPT) blade. The influence of blowing position and frequency on the boundary ...
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    Investigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part II: Experimental Validation 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 008:;page 81010
    Author(s): Niewoehner, Jens; Poehler, Thorsten; Jeschke, Peter; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper is the second part of a twopart paper reporting on the increase in efficiency of a 1.5 stage axial test rig turbine with the use of nonaxisymmetric endwalls and 3D airfoil design. Contoured endwalls were developed ...
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    Investigation of Nonaxisymmetric Endwall Contouring and Three Dimensional Airfoil Design in a 1.5 Stage Axial Turbine—Part I: Design and Novel Numerical Analysis Method 

    Source: Journal of Turbomachinery:;2015:;volume( 137 ):;issue: 008:;page 81009
    Author(s): Poehler, Thorsten; Niewoehner, Jens; Jeschke, Peter; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of the analysis of different 3D designs for the first stator and the rotor of a 1.5stage turbine test rig. A tangential endwall contouring for the hub and the shroud, a bowed profile stacking, ...
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    Loss Mechanisms of Interplatform Steps in a 1.5-Stage Axial Flow Turbine 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 003:;page 31007
    Author(s): Kluxen, Robert; Behre, Stephan; Jeschke, Peter; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the detailed steady and unsteady numerical investigations of a 1.5-stage axial flow turbine are conducted to determine the specific influence of interplatform steps in the first stator—as caused by deviations ...
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    Blade–Row Interactions in a Low Pressure Turbine at Design and Strong Off Design Operation 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 011:;page 111002
    Author(s): Lipfert, Martin; Habermann, Jan; Rose, Martin G.; Staudacher, Stephan; Guendogdu, Yavuz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In a joint project between the Institute of Aircraft Propulsion Systems (ILA) and MTU Aero Engines, a twostage low pressure turbine is tested at design and strong offdesign conditions. The experimental data taken in the ...
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    On Turbulence Measurements and Analyses in a Two-Stage Two-Spool Turbine Rig 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 007:;page 71008
    Author(s): Bauinger, Sabine; Behre, Stephan; Lengani, Davide; Guendogdu, Yavuz; Heitmeir, Franz; Goettlich, Emil
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Since the experiment in turbulence research is of very high importance for evaluating turbulence hypothesis, turbulence measurements were carried out in a two-stage two-spool transonic turbine test rig at the Institute for ...
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