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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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    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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