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    Measurements of Radial Vortices, Spill Forward, and Vortex Breakdown in a Transonic Compressor 

    Source: Journal of Turbomachinery:;2018:;volume 140:;issue 006:;page 61004
    Author(s): Brandstetter, Christoph; Jüngst, Maximilian; Schiffer, Heinz-Peter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The phenomena prior to rotating stall were investigated in a high-speed compressor test rig using optical and pneumatic measurement techniques. A number of throttling procedures were performed at transonic and subsonic ...
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    Compressible Modal Instability Onset in an Aerodynamically Mistuned Transonic Fan 

    Source: Journal of Turbomachinery:;2019:;volume( 141 ):;issue: 003:;page 31004
    Author(s): Brandstetter, Christoph; Paoletti, Benoit; Ottavy, Xavier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes observed modal oscillations arising from a feedback mechanism between an acoustic resonance in the exit flow channel and aerodynamic and aeroelastic disturbances in a transonic fan stage. During tests, ...
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    Acoustic Resonance in an Axial Multistage Compressor Leading to Non-Synchronous Blade Vibration 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 009:;page 091014-1
    Author(s): Fiquet, Anne-Lise; Aubert, Stéphane; Brandstetter, Christoph; Buffaz, Nicolas; Vercoutter, Agathe
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Significant non-synchronous blade vibrations (NSVs) have been observed in an experimental three-stage high-speed compressor at part-speed conditions. High-amplitude acoustic modes, propagating around the circumference and ...
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    UHBR Open-Test Case Fan ECL5/CATANA: Non-Linear Analysis of Non-Synchronous Blade Vibration at Part-Speed Conditions 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 007:;page 71003-1
    Author(s): Fiquet, Anne-Lise; Ottavy, Xavier; Brandstetter, Christoph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The onset of non-synchronous vibrations has been predicted for a composite open-test-case UHBR fan geometry by time-linearized simulations at part-speed conditions. In the current study, time-accurate simulations with ...
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    Unsteady Measurements of Periodic Effects in a Transonic Compressor With Casing Treatments 

    Source: Journal of Turbomachinery:;2016:;volume( 138 ):;issue: 005:;page 51007
    Author(s): Brandstetter, Christoph; Wartzek, Fabian; Werner, Jan; Schiffer, Heinz; Heinichen, Frank
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Application of nonaxisymmetric casing treatments (CTs) can extend the operating range of a transonic compressor significantly. Recent CT designs have proven successful at achieving operating range extension without efficiency ...
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    Aerodynamic Investigation of a Composite Low-Speed Fan for UHBR Application 

    Source: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 010:;page 0101004-1
    Author(s): Rodrigues, Martin; Soulat, Laurent; Paoletti, Benoit; Ottavy, Xavier; Brandstetter, Christoph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A composite fan stage representative of a modern Ultra High Bypass Ratio (UHBR) architecture has been investigated experimentally on a novel test facility at Ecole Centrale de Lyon. These measurements show indications for ...
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    Experiments on Tuned UHBR Open-Test-Case Fan ECL5/CATANA: Stability Limit 

    Source: Journal of Engineering for Gas Turbines and Power:;2023:;volume( 146 ):;issue: 005:;page 51011-1
    Author(s): Brandstetter, Christoph; Fiquet, Anne-Lise; Schneider, Alexandra P.; Paoletti, Benoit; Ottavy, Xavier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Research of the past decades has shown that the operating range of modern fans and compressors is often limited by aeroelastic phenomena before the onset of pure aerodynamic instability. Prediction of these mechanisms is ...
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    Experiments on Tuned UHBR Open-Test-Case Fan ECL5/CATANA: Performance and Aerodynamics 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 008:;page 81001-1
    Author(s): Schneider, Alexandra P.; Fiquet, Anne-Lise; Paoletti, Benoit; Ottavy, Xavier; Brandstetter, Christoph
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: With the advancement of modern fan architectures, the lack of experimental benchmarks for the research community became apparent in the recent years. Enormous effort in the method development could not be validated on ...
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    Experiments on Structurally Mistuned UHBR Open-Test-Case Fan ECL5/CATANA 

    Source: Journal of Engineering for Gas Turbines and Power:;2025:;volume( 147 ):;issue: 008:;page 81010-1
    Author(s): Brandstetter, Christoph; Schneider, Alexandra P.; Fiquet, Anne-Lise; Paoletti, Benoit; Ottavy, Xavier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The operational capabilities of turbofan engines encounter limitations due to instabilities arising from tightly coupled interactions among aerodynamics, acoustics, and structural mechanics. Modern fans and compressors ...
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    Mechanism of Nonsynchronous Blade Vibration in a Transonic Compressor Rig 

    Source: Journal of Turbomachinery:;2017:;volume( 139 ):;issue: 001:;page 11002
    Author(s): Möller, Daniel; Jüngst, Maximilian; Holzinger, Felix; Brandstetter, Christoph; Schiffer, Heinz-Peter; Leichtfuß, Sebastian
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a numerical study on blade vibration for the transonic compressor rig at the Technische Universität Darmstadt (TUD), Darmstadt, Germany. The vibration was experimentally observed for the second eigenmode ...
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