Skip to main content
Log in

Analysis of hot-wire anemometry data in an acoustically excited turbulent flow field

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

Abstract

This paper describes measurements undertaken on an isothermal facility to study the effects of acoustic excitation on the flow field issuing from gas turbine style fuel injectors. The highly swirling and turbulent flow field is excited with plane acoustic waves generated by loudspeakers. Emphasis is placed on the accuracy of the measured response, over the range of excitation frequencies (50–1,500 Hz), and its possible contamination by the background turbulence. Simulated data are used to assess the experimental accuracy and the established errors, using this technique, are compared with an example set of 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

Similar content being viewed by others

Abbreviations

C :

Coherence

D :

Injector diameter

f :

Frequency

G :

Power spectral coefficients

H :

Frequency response function

ΔP :

Pressure drop across fuel injector (time averaged)

pac :

Acoustic fluctuating (rms) pressure

r :

Radius

Tu:

Turbulence intensity (u′/U)

U :

Velocity (time averaged)

uex :

Fluctuating (rms) velocity response to applied excitation

uac :

Acoustic fluctuating (rms) velocity

uqs :

Fluctuating (rms) quasi-steady velocity (Eq. 1)

usim :

Simulated fluctuating (rms) velocity

X :

Axial coordinate

HWA:

Hot wire anemometer

1:

Reference pressure signal

2:

Velocity signal

References

  • Anderson TJ, Kendrick DW, Cohen JM (1998) Measurement of spray/acoustic coupling in gas turbine fuel injectors. AIAA Paper 98-0718, 36th AIAA Aerospace sciences meeting and exhibit

  • Biron D, Simon F (2002) Characteristics of acoustic sources. Muscles report, Onera

    Google Scholar 

  • Bruun H (1995) Hot wire anemometry. Oxford University Press, New York

    Google Scholar 

  • Crow SC, Champagne FH (1971) Orderly structure in jet turbulence. J Fluid Mech 48(3):547–591

    Article  Google Scholar 

  • Eckstein J, Freitag E, Hirsch C, Sattelmayer T (2003) Forced low frequency spray characteristics to a generic airblast swirl diffusion burner. ASME-GT-2003-38646

  • Ho CM, Heurre P (1984) Perturbed free shear layers. Ann Rev Fluid Mech 16:365–424

    Article  Google Scholar 

  • Kroeff G, Carrotte J (2002) Fuel injector studies. Department of Aero Engineering, Loughborough University, UK, University Research Paper TT02R05

  • Lynn PA (1982) An introduction to the analysis and processing of signals. Macmillan, London

    Google Scholar 

  • Marrot F, Simon F, Gajan P, Pauzin S (2000) Active control of a backward-facing step flow. AIAA/CEAS Aeroacoustics conference and exhibit, AIAA-2000-1929

  • Paschereit CO, Wygnanski I, Fiedler HE (1995) Experimental investigation of subharmonic resonance in an axisymetric jet. J Fluid Mech 283:365–407

    Article  Google Scholar 

  • Seybert AF, Soenarko B (1981) Error analysis of spectral estimates with application to the measurement of acoustic parameters using random sound fields in ducts. J Acoust Soc Am 69(4):1190–1199

    Article  MATH  Google Scholar 

  • Shadow KC, Wilson KJ, Gutmark E (1987) Characterisation of large-scale structures in a fored ducted Dflow with dump. AIAA J 25(9):1164–1170

    Article  Google Scholar 

  • Taghavi R, Rice EJ, Farokhi S (1988) Controlled excitation of a cold turbulent swirling free jet. J Vib Acoust Stress Reliability Des Trans ASME110:234–237

    Google Scholar 

  • Zhu M, Dowling AP, Bray KNC (2001) Self excited oscillations in combustors with spray atomizers. Trans ASME J Eng Gas Turbines Power 123:779–786

    Article  Google Scholar 

Download references

Acknowledgements

The authors would like to acknowledge the financial support of the European Union under the MUSCLES framework 5 programme (contract number GRD1-2001-40198). In addition the authors would also like to acknowledge the advice of Alex Riley and Jeff Eldridge (formerly of Cambridge University) for advice on using the two-microphone technique along with some example software.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to J. Carrotte.

Rights and permissions

Reprints and permissions

About this article

Cite this article

Barker, A., Carrotte, J. & Denman, P. Analysis of hot-wire anemometry data in an acoustically excited turbulent flow field. Exp Fluids 39, 1061–1070 (2005). https://doi.org/10.1007/s00348-005-0039-z

Download citation

  • Received:

  • Revised:

  • Accepted:

  • Published:

  • Issue Date:

  • DOI: https://doi.org/10.1007/s00348-005-0039-z

Keywords

Navigation