Skip to main content

Noise Predictions of the Advanced Noise Control Fan Using a Lattice Boltzmann Method and Ffowcs Williams–Hawkings Analogy

  • Conference paper
  • First Online:
Instability and Control of Massively Separated Flows

Part of the book series: Fluid Mechanics and Its Applications ((FMIA,volume 107))

  • 2071 Accesses

Abstract

The purpose is to simulate numerically the flow and noise on the Advanced Noise Control Fan (ANCF). The ANCF model was developed by the NASA Glenn Research Center to provide measurement data of a turbofan flow and its corresponding generated noise. The aim of the numerical simulations is to predict accurately the tonal noise as well as the broadband content of the ducted rotor/stator model using as a reference the provided far-field noise measurements.

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

Access this chapter

Chapter
USD 29.95
Price excludes VAT (USA)
  • Available as PDF
  • Read on any device
  • Instant download
  • Own it forever
eBook
USD 84.99
Price excludes VAT (USA)
  • Available as EPUB and PDF
  • Read on any device
  • Instant download
  • Own it forever
Softcover Book
USD 109.99
Price excludes VAT (USA)
  • Compact, lightweight edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info
Hardcover Book
USD 109.99
Price excludes VAT (USA)
  • Durable hardcover edition
  • Dispatched in 3 to 5 business days
  • Free shipping worldwide - see info

Tax calculation will be finalised at checkout

Purchases are for personal use only

Institutional subscriptions

References

  1. McAllister J, Loew RA, Lauer JT, Sutliff DL (2009) 47th Aerospace sciences meeting and exhibit. Paper number AIAA 2009-0624

    Google Scholar 

  2. Mann A, Perot F, Kim M, Casalino D, Fares E (2012) 18th AIAA/CEAS Aeroacoustics conference and exhibit). Paper number AIAA 2012-2287

    Google Scholar 

  3. Chen S, Doolen GD (1998) Lattice Boltzmann method for fluid flows. Ann Rev Fluid Mech 30:329

    Google Scholar 

  4. Li Y (2012) An improved volumetric LBM boundary approach and its extension for sliding mesh simulation. Ph.D. thesis, Iowa State University

    Google Scholar 

  5. Brés G, Perot F, Freed D (2010) 16th AIAA/CEAS aeroacoustics conference. Paper AIAA 2010-3711 . Stockholm, Sweden

    Google Scholar 

  6. Loew RA, Lauer JT, McAllister J, Sutliff DL (2006) 36th AIAA fluid dynamic conference and exhibit, San Francisco. Paper number AIAA 2006-3150

    Google Scholar 

  7. Pérot F, Kim M, Moreau S, Henner M, Neal D (2010) 16th AIAA/CEAS aeroacoustics conference and exhibit. Paper number AIAA 2010-3887

    Google Scholar 

  8. Hughes C, Woodward R, Podboy G (2005) 11th AIAA/CEAS aeroacoustics conference. Paper AIAA 2005-2875 . Monterey, California

    Google Scholar 

  9. Smith MJT (1989) Aircraft noise. Cambridge University Press, Cambridge

    Google Scholar 

Download references

Acknowledgments

The authors acknowledge CNPq, FINEP and EMBRAER for their financial support. We thank Daniel L. Sutliff from NASA Glenn Research Center for the experimental data.

Author information

Authors and Affiliations

Authors

Corresponding author

Correspondence to B. S. Carmo .

Editor information

Editors and Affiliations

Rights and permissions

Reprints and permissions

Copyright information

© 2015 Springer International Publishing Switzerland

About this paper

Cite this paper

Orselli, R.M., Carmo, B.S., Meneghini, J.R., Queiroz, R.L., Bonatto, A.S. (2015). Noise Predictions of the Advanced Noise Control Fan Using a Lattice Boltzmann Method and Ffowcs Williams–Hawkings Analogy. In: Theofilis, V., Soria, J. (eds) Instability and Control of Massively Separated Flows. Fluid Mechanics and Its Applications, vol 107. Springer, Cham. https://doi.org/10.1007/978-3-319-06260-0_36

Download citation

  • DOI: https://doi.org/10.1007/978-3-319-06260-0_36

  • Published:

  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-06259-4

  • Online ISBN: 978-3-319-06260-0

  • eBook Packages: EngineeringEngineering (R0)

Publish with us

Policies and ethics