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    Variable Cycle Engine Concepts and Component Technologies—An Overview 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 147 ):;issue: 005:;page 51004-1
    Author(s): Zenkner, Sebastian; Carvalho, Francisco; Brakmann, Robin G.; Goinis, Georgios
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The variable cycle engine (VCE) is of interest for military and supersonic civil platforms due to its improved operational flexibility. However, the increase in design and control degrees-of-freedom results in a more complex ...
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    Investigating the Unsteady Dynamics of a Multi-Jet Impingement Cooling Flow Using Large Eddy Simulation 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 003:;page 31002-1
    Author(s): Morsbach, Christian; Matha, Marcel; Brakmann, Robin G.; Tabassum, Sadiya; Bergmann, Michael; Schroll, Michael; Willert, Christian; Kügeler, Edmund
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: We investigate the unsteady behavior of an in-line jet impingement array of nine jets at a Reynolds number of 10,000 in a narrow channel subjected to a developing cross flow of up to 25% of the bulk jet velocity. To this ...
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    Fluidic Oscillators in Impingement Jet Cooling: A Novel Configuration for Realizing Sweeping Jets 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:006:;page 1
    Author(s): Brakmann, Robin G.; Carvalho, Francisco; Matha, Marcel; Morsbach, Christian; Pain, Camille; Pellé, Julien; Rairoux, Emilie; Schroll, Michael; Techen, Erik; Willert, Christian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. This study examines integrating fluidic oscillators into a multi-jet impingement cooling system for turbomachinery, aiming to enhance heat transfer while reducing coolant requirements. The investigated configuration ...
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    Pre-Design and Analysis of a Military Hybrid High-Pressure Turbine 

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:004:;page 487
    Author(s): Carvalho, Francisco; Wehrel, Patrick; Matuschek, Tomasz; Schöffler, Robin; Brakmann, Robin G.; Behrendt, Thomas; Ebel, Paul-Benjamin; Schulz, Uwe; Herbst, Florian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Increasing aero-engine turbine inlet temperatures and stagnating operational limits of nickel-based superalloys creates the need for new materials and cooling technologies. Ceramic matrix composites (CMCs) can ...
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    Wind Tunnel Testing at TRL4 of EBC-Coated SIC/SIC Nozzle Guide Vanes for High-Pressure Turbines With Trailing Edge Cooling 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:005:;page 513
    Author(s): Petersen, Anna; Dimond, Benjamin; Söhngen, Anna-Samira; Süß, Fabia; Ebach-Stahl, Andrea; Naraparaju, Ravisankar; Hilfer, Michael; Brakmann, Robin G.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. To fulfill the high flight requirements for a significantly lower environmental impact, new approaches to the design of engines are required. One solution to build an engine as a whole more efficiently is the use ...
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    Assessment of Computational Fluid Dynamic Modeling of Multi-Jet Impingement Cooling and Validation With the Experiments 

    Source: Journal of Turbomachinery:;2023:;volume( 145 ):;issue: 007:;page 71005-1
    Author(s): Tabassum, Sadiya; Hilfer, Michael; Brakmann, Robin G.; Morsbach, Christian; Willert, Christian; Matha, Marcel; Schroll, Michael
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The current study involves numerical and experimental investigations of circular in-line jets impinging on a heated flat plate. The generic configuration is characterized by nine jets, each with a diameter of D = 0.0152 ...
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