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    Experimental Analysis of the Interaction Between Rim Seal and Main Annulus Flow in a Low Pressure Two Stage Axial Turbine 

    Source: Journal of Turbomachinery:;2013:;volume( 135 ):;issue: 005:;page 51003
    Author(s): Schrewe, Sebastian; Werschnik, Holger; Schiffer, Heinz
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The spoiling effects of rim seal flow are studied at the Large Scale Turbine Rig (LSTR) at Technische Universitأ¤t Darmstadt. Detailed flow field measurements and efficiency measurements were performed for various ingress ...
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    Influence of Combustor Swirl on Endwall Heat Transfer and Film Cooling Effectiveness at the Large Scale Turbine Rig 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 008:;page 81007
    Author(s): Werschnik, Holger; Hilgert, Jonathan; Wilhelm, Manuel; Bruschewski, Martin; Schiffer, Heinz-Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: At the large scale turbine rig (LSTR) at Technische Universität Darmstadt, Darmstadt, Germany, the aerothermal interaction of combustor exit flow conditions on the subsequent turbine stage is examined. The rig resembles a ...
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