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    Combustion Instability and Emission Control by Pulsating Fuel Injection 

    Source: Journal of Turbomachinery:;2008:;volume( 130 ):;issue: 001:;page 11012
    Author(s): Christian Oliver Paschereit; Ephraim Gutmark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Open-loop control methodologies were used to suppress symmetric and helical thermoacoustic instabilities in an experimental low-emission swirl-stabilized gas-turbine combustor. The controllers were ...
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    Tuning of the Acoustic Boundary Conditions of Combustion Test Rigs With Active Control: Extension to Actuators With Nonlinear Response 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 009:;page 91503
    Author(s): Mirko R. Bothien; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the design process, new burners are generally tested in combustion test rigs. With these experiments, as well as with computational fluid dynamics, finite element calculations, and low-order ...
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    Assessment of Different Actuator Concepts for Acoustic Boundary Control of a Premixed Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 002:;page 21502
    Author(s): Mirko R. Bothien; Jonas P. Moeck; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the design process, new burners are generally tested in combustion test rigs. With these experiments, computational fluid dynamics, and finite element calculations, the burners’ performance in ...
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    Combustion Control by Vortex Breakdown Stabilization 

    Source: Journal of Turbomachinery:;2006:;volume( 128 ):;issue: 004:;page 679
    Author(s): Christian Oliver Paschereit; Peter Flohr; Ephraim J. Gutmark
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Flame anchoring in a swirl-stabilized combustor occurs in an aerodynamically generated recirculation region which is a result of vortex breakdown (VBD). The characteristics of the recirculating ...
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    An Experimental Investigation of the Nonlinear Response of an Atmospheric Swirl-Stabilized Premixed Flame 

    Source: Journal of Engineering for Gas Turbines and Power:;2011:;volume( 133 ):;issue: 010:;page 101502
    Author(s): Sebastian Schimek; Jonas P. Moeck; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Due to stringent emission restrictions, modern gas turbines mostly rely on lean premixed combustion. Since this combustion mode is susceptible to thermoacoustic instabilities, there is a need for ...
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    Acoustic Response of a Helmholtz Resonator Exposed to Hot-Gas Penetration and High Amplitude Oscillations 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 010:;page 101503
    Author(s): Bernhard Ćosić; Thoralf G. Reichel; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Helmholtz resonators are often used in the gas turbine industry for the damping of thermoacoustic instabilities. To prevent thermal destruction, these devices are usually cooled by a purging ...
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    Effects of Outlet Boundary Conditions on the Reacting Flow Field in a Swirl-Stabilized Burner at Dry and Humid Conditions 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 011:;page 111501
    Author(s): Steffen Terhaar; Bernhard C. Bobusch; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: During the design and testing process of swirl-stabilized combustors, it is often impractical to maintain identical outlet boundary conditions. Furthermore, it is a common practice to intentionally ...
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    Comparison of Linear Stability Analysis With Experiments by Actively Tuning the Acoustic Boundary Conditions of a Premixed Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 012:;page 121502
    Author(s): Mirko R. Bothien; Jonas P. Moeck; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Linear stability analysis by means of low-order network models is widely spread in industry and academia to predict the thermoacoustic characteristics of combustion systems. Even though a vast ...
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    Thermoacoustic Modeling of a Gas Turbine Combustor Equipped With Acoustic Dampers 

    Source: Journal of Turbomachinery:;2005:;volume( 127 ):;issue: 002:;page 372
    Author(s): Valter Bellucci; Christian Oliver Paschereit; Bruno Schuermans; Dariusz Nowak; Peter Flohr
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this work, the TA3 thermoacoustic network is presented and used to simulate acoustic pulsations occurring in a heavy-duty ALSTOM gas turbine. In our approach, the combustion system is ...
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    Instability Control by Premixed Pilot Flames 

    Source: Journal of Engineering for Gas Turbines and Power:;2010:;volume( 132 ):;issue: 004:;page 41501
    Author(s): Peter Albrecht; Ephraim Gutmark; Stefanie Bade; Arnaud Lacarelle; Christian Oliver Paschereit
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Premixed flames of swirl-stabilized combustors (displaced half-cone) are susceptible to thermo-acoustic instabilities, which should be avoided under all operating conditions in order to guarantee a ...
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