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    Forced Response of an Unstable Low Pressure Turbine Bladed Disk: New States With Different Blade Vibration Amplitude 

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:001
    Author(s): Martel, Carlos; Rodríguez-Blanco, Salvador; González-Monge, Javier
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In the forcing of a low-pressure turbine (LPT) bladed disk, the final amplitude of the vibration state that sets in is determined by the dissipation produced by the friction forces at the blade-disk contact ...
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    Reduced-Order Modeling of Rotor Blades With Geometric Uncertainties 

    Source: Journal of Engineering for Gas Turbines and Power:;2026:;volume( 148 ):;issue:003
    Author(s): Bouras, Abdelhakim; González-Monge, Javier; Carassale, Luigi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. Turbomachinery blade geometry deviates from design specifications because of the manufacturing process or degradation. These represent a source of mistuning, which can cause mode localization and amplified forced ...
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    Conceptual Analysis on the Impact of Acoustic Liners in Fan Flutter 

    Source: Journal of Turbomachinery:;2024:;volume( 147 ):;issue: 004:;page 41001-1
    Author(s): González-Monge, Javier; Pérez, José Miguel; Corral, Roque; Zhao, Fanzhou; Vahdati, Mehdi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work investigates the impact of acoustically treated intakes on fan flutter. The propagation of the fan acoustic perturbations is studied using a simplified model, where the frequency of the waves in the intake is the ...
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