Skip to main content
Log in

Atmospheric low swirl burner flow characterization with stereo PIV

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

Abstract

The lean premixed prevaporized (LPP) burner concept is now used in most of the new generation gas turbines to reduce flame temperature and pollutants by operating near the lean blow-off limit. The common strategy to assure stable combustion is to resort to swirl stabilized flames in the burner. Nevertheless, the vortex breakdown phenomenon in reactive swirling flows is a very complex 3D mechanism, and its dynamics are not yet completely understood. Among the available measurement techniques to analyze such flows, stereo PIV (S-PIV) is now a reliable tool to quantify the instantaneous three velocity components in a plane (2D–3C). It is used in this paper to explore the reactive flow of a small scale, open to atmosphere, LPP burner (50 kW). The burner is designed to produce two distinct topologies (1) that of a conventional high swirl burner and (2) that of a low swirl burner. In addition, the burner produces a lifted flame that allows a good optical access to the whole recirculation zone in both topologies. The flow is studied over a wide range of swirl and Reynolds numbers at different equivalence ratios. Flow statistics are presented for 1,000 S-PIV snapshots at each configuration. In both reactive and cold nonreactive flow, stability diagrams define the domains of the low and high swirl topologies. Due to the relatively simple conception of the physical burner, this information can be easily used for the validation of CFD computations of the burner flow global structure. Near field pressure measurements reveal the presence of peaks in the power spectra, which suggests the presence of periodical coherent features for almost all configurations. Algorithms have been developed to identify and track large periodic traveling coherent structures from the statistically independent S-PIV realizations. Flow temporal evolution is reconstructed with a POD-based method, providing an additional tool for the understanding of flow topologies and numerical codes validation.

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
Fig. 12

Similar content being viewed by others

References

  • Ben Chiekh M, Michard M, Grosjean N, Bera JC (2004) Reconstruction temporelle d’un champ aérodynamique instationnaire à partir de measures PIV non résolues dans le temps. In: 9 Congrès Francophone de Vélocimétrie Laser, Université libre de Bruxelles, Bruxelles, Belgium, 14–17 September 2004

  • Berkooz G, Holmes P, Lumley JL (1993) The proper orthogonal decomposition in the analysis of turbulent flows. Annu Rev Fluid Mech 25:539–575

    Article  MathSciNet  Google Scholar 

  • Birch SF, Khritov KM, Maslov VP, Mironov AK, Secundov AN (2005) An experimental study of flow asymmetry in co-axial jets. 11th AIAA/CEAS aeroacoustics conference (26th AIAA aeroacoustics conference), Monterey, California

  • Cala CE, Fernandes EC, Heitor MV, Shtork SI (2006) Coherent structures in unsteady swirling jet flow. Exp Fluids 40:267–276

    Article  Google Scholar 

  • Cheng RK (1995) Velocity and scalar characteristics of premixed turbulent flames stabilized by weak swirl. Combust Flame 101:1–14

    Article  Google Scholar 

  • Cheng RK, Littlejohn D (2008) Laboratory studies of the flow field characteristics of low swirl injectors for adaptation to fuel-flexible turbines. J Eng Gas Turbines Power 130:021501

    Article  Google Scholar 

  • Cheng RK, Yegian DT, Miyasato MM, Samuelsen GS, Pellizzari R, Loftus P, Benson C (2000) Scaling and development of low-swirl burners for low-emission furnaces and boilers. Proc Combust Inst 28:1305–1313

    Article  Google Scholar 

  • Gupta AK, Lilley DG, Syred N (1984) Swirl flows. ABACUS. ISBN 0-85626-175-0

  • Hjemfelt AT, Mockros LF (1996) Motion of discrete particles in a turbulent fluid. Appl Sci Res 16:149

    Article  Google Scholar 

  • Kähler CJ, Sammler BS, Kompenhans JK (2001) Generation and control of particle size distributions for optical velocity measurement techniques in fluid mechanics. 4th international symposium on PIV, Gottingen, Germany

  • Kostas J, Soria J, Chong MS (2005) A comparison between snapshot POD analysis of PIV velocity and vorticity data. Exp Fluids 38:146–160

    Article  Google Scholar 

  • Legrand M (2008) Estudio y caracterización de un quemador estabilizado con giro. PhD Thesis. Universidad Carlos III de Madrid, Spain

  • Lucca-Negro O, O’Doherty T (2001) Vortex breakdown: a review. Prog Energy Combust Sci 7:431–481

    Article  Google Scholar 

  • Malalasekera W, Ranga Dinesh KKJ, Ibrahim SS, Kirkpatrick P (2007) Large eddy simulation of isothermal turbulent swirling jet. Combust Sci Technol 179(8):1481–1525

    Article  Google Scholar 

  • Meyer KE, Cavar D, Pedersen JM (2007) POD as tool for comparison of PIV and LES data. 7th international symposium on particle image velocimetry. Rome, Italy

  • Nauri S, Legrand M, Lecuona A, Rodríguez PA, Nogueira J (2006) Combination of advanced 2D PIV and stereo technique. 13th International symposium on applications of laser techniques to fluid mechanics, Lisbon, Portugal

  • Nauri S, Nogueira J, Lecuona A, Legrand M, Rodríguez PA (2008) Limits and accuracy of the stereo LFC-PIV Technique and its application to flows of industrial interest. Exp Fluids 45/4:609–621

    Article  Google Scholar 

  • Nogueira J, Legrand M, Nauri S, Rodríguez PA, Lecuona A (2008) Analysis of the vortex street generated at the core bypass lip of a jet engine nozzle. Top Appl Phys 112:419–428

    Article  Google Scholar 

  • Nogueira J, Lecuona A, Nauri S, Legrand M, Rodríguez PA (2009) Multiple Δt strategy for particle image velocimetry (PIV) error correction, applied to a hot propulsive jet. Meas Sci Technol 20(7):074001

    Google Scholar 

  • Perrin R, Braza M, Cid E, Cazin S, Barthet A, Sevrain A, Mockett C, Thiele F (2007) Obtaining phase averaged turbulence properties in the near wake of a circular cylinder at high reynolds number using POD. Exp Fluids 43:341–355

    Article  Google Scholar 

  • Petersson P, Olofsson P, Brackman C, Seyfried C, Zetterberg J, Richter M, Aldén M, Linne MA, Cheng RK, Nauert A, Geyer D, Dreizler A (2007) Simultaneous PIV/OH-PLIF, Rayleigh thermometry/OH-PLIF and stereo PIV measurements in a low-swirl flame. Appl Opt 46(19):3928–3936

    Article  Google Scholar 

  • Raffel M, Willert CE, Kompenhans J (2000) Particle imaging velocimetry: a practical guide. Springer, Dordrecht, pp 179–184

    Google Scholar 

  • Sarpkaya T (1971) On stationary and traveling vortex breakdowns. J Fluid Mech 45(3):545–590

    Article  Google Scholar 

  • Sirovich L (1987) Turbulence and the dynamics of coherent structures, Parts I, II and III. Q Appl Math 45(3):561–582

    MATH  MathSciNet  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 unsteady flow

    Article  Google Scholar 

  • Van Oudheusden BW, Scarano F, Van Hinsberg NP, Watt DW (2005) Phase-resolved characterization of vortex shedding in the near wake of a square section cylinder at incidence. Exp Fluids 39:86–98

    Article  Google Scholar 

  • Wall TF (1987) The combustion of coal as pulverized fuel through Swirl Burners, Chapter 3. In: Lawn CJ (ed) Principles of combustion engineering for boilers. Academic Press, London

    Google Scholar 

  • Wieneke B (2005) Stereo-PIV using self-calibration on particle images. Exp Fluids 39:267–280

    Article  Google Scholar 

  • Willert C (1997) Stereoscopic digital image particle velocimetry for application in wind tunnel flows. Meas Sci Technol 8:1465–1479

    Article  Google Scholar 

  • Zeldovich YB, Sadovnikov PY, Frank-Kamenetskii DA (1947) Oxidation of nitrogen in combustion. Acad Sci, USSR, Moscow-Leningrad

Download references

Acknowledgments

This work has been partially funded by the CoJeN European project, Specific Targeted RESEARCH Project EU Contract No. AST3-CT-2003-502790; the Spanish Research Agency grant DPI2002-02453 “Técnicas avanzadas de Velocimetría por Imagen de Partículas (PIV) Aplicadas a Flujos de Interés Industrial”, the Spanish Research Agency grant ENE2006-13617 “TERMOPIV: Combustión y transferencia de calor analizadas con PIV avanzado” and the Madrid community grant “CCG08-UC3M/ENE-4432”. We would like also to express a special acknowledgement to the laboratory technicians Manuel Santos and Carlos Cobos, for their help in the burner design and manufacture.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to Mathieu Legrand.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Legrand, M., Nogueira, J., Lecuona, A. et al. Atmospheric low swirl burner flow characterization with stereo PIV. Exp Fluids 48, 901–913 (2010). https://doi.org/10.1007/s00348-009-0775-6

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00348-009-0775-6

Keywords

Navigation