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    Reducing Low-Pressure Turbine Shroud Leakage Loss by Optimizing Leakage-Mainstream Interaction 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:005:;page 1
    Author(s): Camarero Pueyo, Josué-Inocente; Helmsen, Eike; Oettinger, Marcel; Klingl, Stefan; Junghans, Haris; Palkus, Kacper; Wein, Lars
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In turbomachinery, mixing in the blade tip region between tip leakage and mainstream flow leads to irreversible entropy production, which is detrimental to efficiency. Despite extensive efforts to reduce leakage ...
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    Maintenance of Jet Engines: Robust Parameterization and Reconstruction of Compressor and Turbine Blades 

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:008:;page 515
    Author(s): Dammann, Maximilian; Schulten, Benedikt; Goeing, Jan; Steiner, Maximilian; Koster, Max; Friedrichs, Jens; Seume, Joerg R.; Wein, Lars
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Maintenance, repair, and overhaul (MRO) of jet engines rely on geometric inspection and aerothermodynamic performance analysis of compressor and turbine blades. In order to analyze the variability of airfoil ...
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    Predicting Endwall Corner Separation in Compressor Cascades Using RANS: Influence of Transition Treatment and Inflow Conditions 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:007
    Author(s): Franke, Pascal; Suchla, Dominik A.; Ottavy, Xavier; Mimic, Dajan; Wein, Lars
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Corner separations are a complex physical phenomenon that significantly affects the off-design operation of axial compressors, contributing to instability and limiting their operating range. At the same time, ...
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