Skip to main content
Log in

Acoustic forcing on swirling flow: experiments and simulation

  • Research Article
  • Published:
Experiments in Fluids Aims and scope Submit manuscript

Abstract

We investigated the effect of sound irradiated from loudspeakers on the flow of preheated air in the combustion chamber of a swirl burner. The temporally periodic pattern of the flow generated by the sound was detected by fast particle image velocimetry (PIV), with a repetition rate that was adapted to the observation of 12 phase angles of the irradiated monochromatic sound. The strong observed movement of the air is related to the movement by the sound itself, as determined by the pressure measurements with microphones. The PIV measurements reveal also a nonlinear interaction between the irradiated sound and the precession of the vortex core. The accuracy of the sound measurements was tested by determining in quiescent air the acoustic velocity by microphones and as well by PIV; good agreement was obtained thereby. Numerical calculations, using large eddy simulation and accounting for the sound forcing by variation in the mass flow at the inlet of the computational domain, approximately reproduce some of the experimental results.

This is a preview of subscription content, log in via an institution to check access.

Access this article

Price excludes VAT (USA)
Tax calculation will be finalised during checkout.

Instant access to the full article PDF.

Fig. 1
Fig. 2
Fig. 3
Fig. 4
Fig. 5
Fig. 6
Fig. 7
Fig. 8
Fig. 9
Fig. 10
Fig. 11

Similar content being viewed by others

References

  • Biagioli F (2006) Stabilization mechanism of turbulent premixed flames in strongly swirled flows. Combust Theory Model 10:389–412

    Article  MathSciNet  MATH  Google Scholar 

  • Biagioli F, Paikert B, Genin F, Noiray N, Bernero S, Syed K (2013) Dynamic response of turbulent low emission flames at different vortex breakdown conditions. Flow Turbul Combust 90:343–372

    Article  Google Scholar 

  • Candel S, Durox D, Schuller T, Palies P, Bourgouin JF, Moeck JP (2012) Progress and challenges in swirling flame dynamics. Compte Rendus Méc 340:758–768

    Article  Google Scholar 

  • Davis JH (1979) Wiener–Hopf methods for open-loop unstable distributed systems. SIAM J Control Optim 17:713–728

    Article  MathSciNet  MATH  Google Scholar 

  • Döbbeling K, Hellat J, Koch H (2005) 25 years of BBC/ABB/Alstom lean premix combustion technologies. In: Proceedings of the ASME Turbo Expo (Paper GT2005-68269)

  • Duan XR, Meier W, Weigand P, Lehmann B (2005) Phase-resolved laser Raman scattering and laser Doppler velocimetry applied to periodic instabilities in a gas turbine model combustor. Appl Phys B80:389–396

    Article  Google Scholar 

  • Giezendanner R, Keck O, Weigand P, Meier W, Meier U, Stricker W, Aigner M (2003) Periodic combustion instabilities in a swirl burner studied by phase-locked planar laser-induced fluorescence. Combust Sci Technol 175:721–741

    Article  Google Scholar 

  • Hauser M, Wagner M, Sattelmayer T (2012) Transformation of transverse acoustic velocity of the burner approach flow into flame dynamics. In: Proceedings of ASME Turbo Expo 2012: GT2012-69051

  • Hosseini SMR, Gardner C, Lawn C (2012) The non-linear thermo-acoustic response of a small swirl burner. Combust Flame 159:1909–1920

    Article  Google Scholar 

  • Hubschmid W, Inauen A, Bombach R, Kreutner W, Schenker S, Zajadatz M, Motz C, Haffner K, Paschereit CO (2002) Sound generating flames of a gas turbine burner observed by laser-induced fluorescence. PSI Scientific Report 2001/Volume V: 57–58. http://cdg.web.psi.ch/

  • Hubschmid W, Bombach R, Inauen A, Güthe F, Schenker S, Tylli N, Kreutner W (2008) Thermoacoustically driven flame motion and heat release variation in a swirl-stabilized gas turbine burner investigated by LIF and chemiluminescence. Exp Fluids 45:167–182

    Article  Google Scholar 

  • Jasaka HH, Weller HG, Gosman AD (1999) High resolution NVD differencing scheme for arbitrarily unstructured meshes. Int J Number Methods Fluids 31:431–449

    Article  Google Scholar 

  • Lawn CJ, Evesque S, Polifke W (2004) A model of the thermoacoustic response of a premixed swirl burner, part I: acoustic aspects. Combust Sci Technlo 178:1331–1368

    Article  Google Scholar 

  • Meier W, Weigand P, Duan XR, Giezendanner R (2007) Detailed characterization of the dynamics of thermoacoustic pulsations in a lean premixed flame. Combust Flame 150:2–26

    Article  Google Scholar 

  • O’Connor J, Lieuwen T (2011) Further characterization of the disturbance field in a transversely excites swirl-stabilized flame. In: Proceedings of ASME Turbo Expo 2011: GT2011-45221

  • O’Connor J, Lieuwen T (2012) Influence of transverse acoustic modal structure on the forced response of a swirling nozzle flow. In: Proceedings of ASME Turbo Expo 2012: GT2012-70053

  • O’Connor J, Lieuwen T (2013) Disturbance field characteristics of a transversely excited burner. Combust Sci Technol 183:427–443

    Article  Google Scholar 

  • Oberleithner K, Sieber M, Nayeri CN, Paschereit CO, Petz C, Hege HC, Noack BR, Wygnanski I (2011) Three-dimensional coherent vortex breakdown: stability analysis and empirical mode construction. J Fluid Mech 679:383–414

    Article  MATH  Google Scholar 

  • Poinsot T, Veynante D (2005) Theoretical and numerical combustion, 2nd edn. Edwards, Philadelphia

    Google Scholar 

  • Schimek S, Cosic B, Moeck JP, Terhaar S, Paschereit CO (2012) Amplitude-dependent flow field and flame response to axial and tangential velocity fluctuations. In: Proceedings of ASME Turbo Expo 2012: GT2012-69785

  • Smagorinsky J (1963) General circulation experiments with the primitive equations. Mon Weather Rev 91:99–164

    Article  Google Scholar 

  • Syred N (2006) A review of oscillation mechanisms and the role of the precessing vortex core (PVC) in swirl combustion systems. Prog Energy Combust Sci 32:93–161

    Article  Google Scholar 

  • Tylli N, Hubschmid W, Inauen A, Bombach R, Schenker S, Güthe F, Haffner K (2005) Flame motion in gas turbine burner from averages of single-pulse flame fronts. PSI Scientific Report 2004/Volume V: 65–66. http://cdg.web.psi.ch/

  • Wehe SD, Li H, McManus KR (2011) Flame transfer function measurements in a single nozzle combustor. In: Proceedings of ASME Turbo Expo 2011: GT2011-45323

  • Weigand P, Meier W, Duan XR, Giezendanner R, Meier U (2005) Laser diagnostic study of the mechanism of a periodic combustion instability in a gas turbine model combustor. Flow Turbul Combust 75:275–292

    Article  MATH  Google Scholar 

Download references

Acknowledgments

We thank Vishal Toro for building up the test rig at PSI and Rafal Slefarski for doing first tests. For maintaining and continuous improving of the test rig, we thank Pascal Beerkircher and Philipp Schmitt. For assistance in performing the LES simulations, we thank Federico Olimpi. Furthermore, we thank P. Jansohn for careful reading of the text and Y. Mantzaras for discussions.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to W. Hubschmid.

Electronic supplementary material

Rights and permissions

Reprints and permissions

About this article

Check for updates. Verify currency and authenticity via CrossMark

Cite this article

Hubschmid, W., Denisov, A. & Biagioli, F. Acoustic forcing on swirling flow: experiments and simulation. Exp Fluids 55, 1808 (2014). https://doi.org/10.1007/s00348-014-1808-3

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • DOI: https://doi.org/10.1007/s00348-014-1808-3

Keywords

Navigation