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    A Statistical Characterization of the Effects and Interactions of Small and Large Mistuning on Multistage Bladed Disks 

    Source: Journal of Engineering for Gas Turbines and Power:;2020:;volume( 142 ):;issue: 004
    Author(s): Kurstak, Eric; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As turbomachinery systems continue to push the limits of modern technology, the modeling techniques being developed also continue to push modern computational limits. While modeling the pristine system during the design ...
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    An Experimental and Computational Investigation of a Pulsed Air-Jet Excitation System on a Rotating Bladed Disk 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 001:;page 011017-1
    Author(s): Kurstak, Eric; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Nonsynchronous vibrations are a difficult problem to address for turbomachines due to the complex nature of the forcing. Such vibrations can be caused by vortex shedding, flow instabilities, stall cells, or flutter. Testing ...
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    Multistage Blisk and Large Mistuning Modeling Using Fourier Constraint Modes and PRIME 

    Source: Journal of Engineering for Gas Turbines and Power:;2018:;volume( 140 ):;issue: 007:;page 72505
    Author(s): Kurstak, Eric; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Current efforts to model multistage turbomachinery systems rely on calculating independent constraint modes for each degree-of-freedom (DOF) on the boundary between stages. While this approach works, it is computationally ...
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    Parametric Study of a Unmanned Aerial Vehicle Ingestion Into a Business Jet Size Fan Assembly Model 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 007:;page 71002
    Author(s): Lyons, Troy; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This work investigated the damage severity of an unmanned aerial vehicle (UAV) ingestion into fan models of a midsized business jet engine. The ingestion of the quadcopter UAV model into the fan was carried out in ls-dyna. ...
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    A Broadband Piezoelectric Energy Harvester With Robust Control Using Piecewise Nonlinearity 

    Source: Journal of Computational and Nonlinear Dynamics:;2025:;volume( 020 ):;issue: 008:;page 81003-1
    Author(s): Guan, Yuqin; D’Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: -
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    Analyzing Bilinear Systems Using a New Hybrid Symbolic-Numeric Computational Method 

    Source: Journal of Vibration and Acoustics:;2019:;volume( 141 ):;issue: 003:;page 31008
    Author(s): Tien, Meng-Hsuan; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, an efficient and accurate computational method for determining responses of high-dimensional bilinear systems is developed. Predicting the dynamics of bilinear systems is computationally challenging since ...
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    Parametric Reduced Order Models for Bladed Disks With Mistuning and Varying Operational Speed 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 005:;page 51018
    Author(s): Kurstak, Eric; Wilber, Ryan; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A considerable amount of research has been conducted to develop reduced order models (ROMs) of bladed disks that can be constructed using single sector calculations when there is mistuning present. A variety of methods ...
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    Parametric Reduced Order Models for Bladed Disks With Mistuning and Varying Operational Speed 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 005:;page 51018
    Author(s): Kurstak, Eric; Wilber, Ryan; D'Souza, Kiran
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: A considerable amount of research has been conducted to develop reduced order models (ROMs) of bladed disks that can be constructed using single sector calculations when there is mistuning present. A variety of methods ...
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    Experimental Determination of Blade Tip Rub Forces in a Multiblade System 

    Source: Journal of Engineering for Gas Turbines and Power:;2022:;volume( 145 ):;issue: 004:;page 41011-1
    Author(s): Reifsnyder, Robin; Keener, Christopher; Mathison, Randall; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As improved efficiency goals require ever smaller gaps between rotating turbomachinery blade tips and stationary outer casings, it becomes more important to understand the physics of what happens when a blade tip rubs ...
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    Efficient Hybrid Symbolic-Numeric Computational Method for Piecewise Linear Systems With Coulomb Friction 

    Source: Journal of Computational and Nonlinear Dynamics:;2023:;volume( 018 ):;issue: 007:;page 71004-1
    Author(s): Shahhosseini, Amir; Tien, Meng-Hsuan; D'Souza, Kiran
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A wide range of mechanical systems have gaps, cracks, intermittent contact or other geometrical discontinuities while simultaneously experiencing Coulomb friction. A piecewise linear model with discontinuous force elements ...
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