24 research outputs found

    Identification of the flame describing function of a premixed swirl flame from les

    Get PDF
    Thermo-acoustic characterization of gas turbine combustion systems is crucial for a successful development of new gas turbine engines to meet emission and efficiency targets. In this context, it becomes more and more necessary to predict the limit cycle amplitudes of thermo-acoustic induced combustion instabilities in order to figure out if they can be tolerated or if they are above the critical design limit and will cause damage to the engine. For the prediction of limit cycle amplitudes, the nonlinear flame response of the combustion system is needed, which is represented in this work by the flame describing function (FDF). In this article, the identification of the FDF from a large eddy simulation (LES) is validated. The test case used was a premixed atmospheric swirl flame, for which experimental data on the FDF were available. First a steady reacting LES solution was obtained and compared to experimental data. The simulation was then excited by superimposing a mono-frequency harmonic wave on the velocity inlet boundary condition. Both the frequency and amplitude of the acoustic wave were varied to obtain the FDF. The calculated FDF was in good agreement with experimental data. At a frequency of 115 Hz, the heat release rate of the flame was found to saturate for larger excitation amplitudes.</p

    Acoustic control of combustion instabilities and emissions in a gas-turbine combustor

    No full text

    Rule Based Control of Combustion Instabilities Using an Adaptive, Fuzzy Algorithm

    No full text

    Numerical studies on the influence of periodical flow forcing on mixing quality and flow structure of a swirl burner

    No full text
    Helical coherent structures and strong axial mass flow fluctuations related to acoustic instabilities are common features in swirl-stabilized gas turbine combustors. The investigation of these dynamical phenomena, in particular their interaction, is therefore important. In the present work, the periodical excitation of the flow field of a swirl burner and its impact on coherent flow structures and mixing properties is examined. The effect of axial mass flow excitation with the dominant frequency of the coherent structure is studied. The investigations are conducted with unsteady RANS (URANS) and Large Eddy simulations (LES) for isothermal conditions to examine their capability of capturing the impact of forcing on the mixing and flow characteristics. Mean and turbulent flow fields as well as the concentration fields at the burner outlet are studied. The mixing quality is characterized by the degree of unmixedness, and the flow structures of the unforced and forced cases are analyzed by proper orthogonal decomposition (POD). With external forcing of the mean flow, the concentration field at the burner outlet becomes more homogeneous, i.e. the mixing quality increases. The unforced flow field exhibits a helical structure, which changes its characteristics when forcing is applied. The simulations (both URANS and LES) are able to reproduce the main features. URANS, however, strongly underpredicts the turbulence intensity in the recirculation zone and shear layers, and as a result, the kinetic energy distribution captured by the POD modes is not in agreement with experimental the findings. The results from LES are qualitatively and also quantitatively in good agreement with the experimental data. Copyright © 2012 by ASME
    corecore