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Study of instabilities in a BRS burner using a Green’s Function Approach

This study delves into analyzing combustion instabilities in a BRS burner by combining the Green’s function method with CFD simulations. The Flame Describing Function, reflection coefficients, and integral equations are employed to understand the response of the system to perturbations. Modal amplitudes, resonant frequencies, governing equations, and heat release models are explored to create stability maps for the burner. The research investigates feedback mechanisms, time-lag distributions, Wiener Hopf Inversion method, and stability analysis for different perturbation amplitudes. The work, supported by the Marie Curie Initial Training Network TANGO, aims to enhance understanding and predict the stability of the BRS burner. Ongoing work includes exploring different heat release models and analyzing losses in the system using reflection coefficients. The study acknowledges financial support from the European Commission and hints at new research topics in optical cavity instabilities.

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Study of instabilities in a BRS burner using a Green’s Function Approach

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  1. Study of instabilities in a BRS burner using a Green’s Function Approach Dr. Alessandra Bigongiari

  2. Introduction: the method • Analysis of the combustion instabilities in a BRS burner combining the Green’s function method with CFD simulations: FLAME RESPONSE TO PERTURBATIONS Flame Describing Function Reflection coefficients Q(t,τ) Reflection coefficients Integral Equation Q,G Acoustic field u Green’s function Q (u) from FDF

  3. Green’s function Response of the system to a point source located in x’ and firing at t’ ωn=resonant frequencies Tailored: same boundary conditions as the acoustic field • Modal amplitudes gn and frequencies ωn are calculated for the BRS GOVERNING EQUATION g1 L 0

  4. Integral equation & heat release model Integral equation derived from: Governing equation for G Acoustic Analogy equation Integral equation derived from: Governing equation for G Acoustic Analogy equation Numerical Iteration FDF calculated from the model Heat release model Time-lag distribution Heat release law: FEEDBACK Low pass filter behaviour

  5. FDF from full CDF simulations (3D) 3D Simulations performed by DmytroIurashev, in the OpenFOAM environment -Different values of the perturbation amplitudes A/U(%) -Wiener Hopf Inversion and single frequency method (for high perturbation amplitudes) Fit using the FDF from our model Heat release law: FEEDBACK

  6. STABILITY MAPS Stability map for the control parameter L (total length). Green=unstable, White=stable Gaussian time-lag distribution Other parameters Sratio= 0.13 (ratio of cross-sectional areas) xj =0.16m(position of the temperature jump) xq = 0.21m (flame position). R0=1 (rigid end), RL =-1(open end) Heater power/mass flow Heat release law: FEEDBACK Discrete time-lag distribution

  7. LOSSES Stability map for the control parameter L (total length). Green=unstable, White=stable Gaussian time-lag Distribution RL=-0.9 Other parameters Sratio= 0.13 (ratio of cross-sectional areas) xj =0.16m(position of the temperature jump) xq = 0.21m (flame position). R0=1 (rigid end) Heater power/mass flow Gaussian time-lag Distribution RL=-0.576-i0.491.

  8. Validation Validation is still in progress. First results show that the system is more stable than map predictions. P(x=21 cm)~Flame position Initial condition lInf=10cm Gaussian time-lag Distribution RL=-0.576-i0.491.

  9. CONCLUSIONS & WORK IN PROGRESS We have produced stability maps for a BRS burner using a Flame Describing Function extracted from full CFD simulations. We have used a heat release model with a distribution of time-lags and produced stability maps. We are studying a different heat release model introducing a distribution for the time-lags where 2 time-lags are considered. Further analysis of losses (described by reflection coefficients) is in progress.

  10. THANKS FOR YOUR ATTENTION The presented work is part of the Marie Curie Initial Training Network Thermo-acoustic and aero-acoustic nonlinearities in green combustors with orifice structures (TANGO). We gratefully acknowledge the financial support from the European Commission under call FP7-PEOPLE-ITN-2012.

  11. My new research topic in Pisa… Instabilities in an optical cavity (with a laser), generated by the delayed response (dilatation) of an irradiated membrane. Pictures represent the instabilities in the transmitted field (green) and the oscillations at the membrane surface (blue)

  12. My new research topic in Pisa… Cavity resonance λ=nL before expansion λ’=n(L-dL) after exp. Ligth cause the thermal expansion of the membrane in a time τ Laser τDelay associated to thermal expansion: I(λ)=light intensity at resonance > thermal expansion with delay τ >cavity resonance condition changes: decay of the intensity until a new resonance condition is reached >contraction of the membrane with delay τ>superposition of waves gives damping or unstability

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